DNEPR 1 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite DNEPR 1 R/B at a glance.

Uptime

8990

Days in orbit

Revolutions

≈ 13.8

Per day

Orbit

LEO

Low Earth Orbit

Inclination

64.6

Latest

Satellite identification and parameters

Extended collection of information and parameters for DNEPR 1 R/B.

Object identification

Identified? True

Debris? False

Object name: DNEPR 1 R/B

International designator: 2000-057F

Object number (NORAD): 26550

Object ID (CCSDS): 26550

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 104.204 minutes

Inclination: 64.563 deg

SMA: 7335.278 km

Apoapsis: 1330.446 km

Periapsis: 583.84 km

RAAN: 308.0486 deg

Eccentricy: 0.0508915

Argument of periapsis: 131.5611 deg

Mean anomaly: 233.0262 deg

Mean motion: 13.81904124 rev/day

Mean motion (dot): 0.00000399 rev/day2

B* drag term: 0.00017528 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 7:16 p.m. UTC

TLE line 0: 0 DNEPR 1 R/B

TLE line 1: 1 26550U 00057F 25127.80295182 .00000399 00000-0 17528-3 0 9999

TLE line 2: 2 26550 64.5630 308.0486 0508915 131.5611 233.0262 13.81904124240668

Live tracking on map

Real-time ground track for satellite DNEPR 1 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object DNEPR 1 R/B.

Target Orbit TCA Probability of collision Miss distance Type
SL-14 R/B LEO 2025-03-24 20:03:39 0.0003898051 734.0 (m) ROCKET BODY
CZ-6A DEB LEO 2024-09-18 07:16:14 0.001896199 343.0 (m) DEBRIS

Associated space launch

Four small satellites were launched atop the Dnepr launch vehicle : MegSat 1, UniSat 1, TiungSat 1 as well as SaudiSat 1a and 1b. MegSat 1 is the second MegSat satellite. It is a LEO communications satellite. UniSat 1 is an Italian satellite developed and operated by GAUSS (La Sapienza University of Rome). TiungSAT-1 or MySat (Malaysian Satellite) is the first microsatellite for the Astronautic Technology (M) SDN. BHD. Company (ATSB) in Kuala Lumpur, Malaysia. Saudisat-1a and Saudisat-1b (Saudi Arabian Satellite) are the first Saudi Arabian micro satellites.

DNEPR 1 R/B was lifted into orbit during the mission ‘Dnepr | SmallSat Rideshare’, on board a Dnepr space rocket.

The launch took place on Sept. 26, 2000, 10:05 a.m. from 109/95.

For more information about the launch, click the button.

Launch to space Dnepr | SmallSat Rideshare
Dnepr | SmallSat Rideshare

Agency: N/A

Status: Launch Successful

Launch date: Sept. 26, 2000, 10:05 a.m. UTC

Rocket: Dnepr

Launch pad: 109/95

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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