Key statistics
Satellite TOMS EP at a glance.
Uptime
10757
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.5
Latest
Satellite identification and parameters
Extended collection of information and parameters for TOMS EP.
Object identification
Identified? True
Debris? False
Object name: TOMS EP
International designator: 1996-037A
Object number (NORAD): 23940
Object ID (CCSDS): 23940
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 98.659 minutes
Inclination: 98.4892 deg
SMA: 7072.679 km
Apoapsis: 713.751 km
Periapsis: 675.338 km
RAAN: 145.312 deg
Eccentricy: 0.00271556
Argument of periapsis: 63.5816 deg
Mean anomaly: 296.8165 deg
Mean motion: 14.59576331 rev/day
Mean motion (dot): 0.00001395 rev/day2
B* drag term: 0.00030245329 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 4:17 a.m. UTC
TLE line 0: 0 TOMS EP
TLE line 1: 1 23940U 96037A 25346.17912157 .00001395 00000-0 30245-3 0 9991
TLE line 2: 2 23940 98.4892 145.3120 0027156 63.5816 296.8165 14.59576331564743
Live tracking on map
Real-time ground track for satellite TOMS EP.
Associated space launch
TOMS EP was lifted into orbit during the mission ‘Pegasus XL | Total Ozone Mapping Spectrometer (TOMS)’, on board a Pegasus XL space rocket.
The launch took place on July 2, 1996, 7:48 a.m. from Vandenberg Space Force Base.
For more information about the launch, click the button.
Pegasus XL | Total Ozone Mapping Spectrometer (TOMS)
Agency: N/A
Status: Launch Successful
Launch date: July 2, 1996, 7:48 a.m. UTC
Rocket: Pegasus XL
Launch pad: Vandenberg Space Force Base
Location: Air launch to orbit
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