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AEPEX

In orbit NORAD 68506 ROGL-5396-9562-5275-1160 United States of America

Time in UTC

08:28

Next pass · Индия · 6°

15.10 11:45

Scheduled · Геоскан

59

Observations over 30 days

54%

Successful observations

26k

Frames, latest 2026-10-15 01:03 UTC

Mission information
Spacecraft name
AEPEX
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Last observers
Observer
Time of receipt
2026-10-15 01:03:12 UTC
2026-10-14 12:13:50 UTC
2026-10-14 01:22:53 UTC
2026-10-13 10:53:27 UTC
2026-10-13 01:41:48 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.17 km
Apogee
504.24 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6879.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68506U 26067CU  26286.83733979  .00007889  00000-0  36365-3 0  9997
2 68506 97.4665 243.9125 0004414 52.3643 307.7992 15.20531002 29845
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 09:18:44 AEPEX
NORAD 68506
STPSAT-7
NORAD 68630
4.207 14.85 9.7e-08
2026-10-15 10:53:19 AEPEX
NORAD 68506
STPSAT-7
NORAD 68630
4.480 14.85 8.6e-08
2026-10-15 11:07:21 AEPEX
NORAD 68506
DMSP 5D-2 F14 DEB
NORAD 62945
3.256 13.24 2.4e-07
2026-10-16 10:55:21 NUSAT-53 (JANE GOODALL)
NORAD 68432
AEPEX
NORAD 68506
2.552 0.01 6.8e-07
2026-10-17 01:49:48 PIAST-M
NORAD 66758
AEPEX
NORAD 68506
3.016 12.71 3.0e-07
2026-10-17 02:34:35 VIREON-1
NORAD 68434
AEPEX
NORAD 68506
1.642 0.00 1.6e-06
2026-10-17 02:37:10 PIAST-M
NORAD 66758
AEPEX
NORAD 68506
4.032 12.68 1.7e-07
2026-10-17 06:34:03 TRANSPORTER-15 OBJECT DM
NORAD 66773
AEPEX
NORAD 68506
2.723 12.73 3.7e-07
2026-10-17 06:50:46 STARLINK-5003
NORAD 53905
AEPEX
NORAD 68506
4.180 14.33 3.5e-06
2026-10-17 07:21:26 TRANSPORTER-15 OBJECT DM
NORAD 66773
AEPEX
NORAD 68506
4.470 12.70 1.4e-07
2026-10-17 08:08:11 OBJECT C
NORAD 65940
AEPEX
NORAD 68506
3.010 13.32 2.8e-07
2026-10-17 10:47:34 STARLINK-5003
NORAD 53905
AEPEX
NORAD 68506
4.689 14.28 2.8e-06
2026-10-17 16:01:52 MACSAT (FINCH 1)
NORAD 58024
AEPEX
NORAD 68506
3.514 13.43 2.0e-07
2026-10-17 16:07:21 STARLINK-4466
NORAD 53656
AEPEX
NORAD 68506
2.082 10.15 2.4e-05
2026-10-17 16:49:15 MACSAT (FINCH 1)
NORAD 58024
AEPEX
NORAD 68506
4.709 13.40 1.1e-07
2026-10-17 16:50:04 AC1-002
NORAD 66745
AEPEX
NORAD 68506
2.565 12.63 4.2e-07
2026-10-17 18:29:31 STARLINK-4466
NORAD 53656
AEPEX
NORAD 68506
0.783 10.13 1.7e-04
2026-10-19 00:30:07 AEPEX
NORAD 68506
CZ-2C DEB
NORAD 37735
2.195 1.17 9.1e-07
2026-10-19 12:46:33 RASSVET-3 9
NORAD 68368
AEPEX
NORAD 68506
3.038 2.08 4.7e-07
2026-10-20 15:56:26 HJ-2E
NORAD 54035
AEPEX
NORAD 68506
3.207 5.77 4.0e-07
2026-10-20 16:32:45 FGN-100-D2
NORAD 66299
AEPEX
NORAD 68506
4.357 10.80 1.7e-07
2026-10-20 16:43:48 HJ-2E
NORAD 54035
AEPEX
NORAD 68506
4.603 5.78 1.9e-07
2026-10-20 19:05:50 OBJECT C
NORAD 61240
AEPEX
NORAD 68506
3.711 6.27 3.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite