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AIGLONSAT-1

In orbit NORAD 68437 SJWO-3715-0167-1613-8791

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
AIGLONSAT-1
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
492.68 km
Apogee
497.58 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6873.3 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 68437U 26067X   26283.63138964  .00019279  00000-0  83236-3 0  9993
2 68437 97.4641 240.9604 0003565 47.3433 312.8103 15.22546208 29496
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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
2026-10-11 14:18:58 STARLINK-5918
NORAD 55939
AIGLONSAT-1
NORAD 68437
4.154 14.38 3.5e-06
2026-10-12 12:26:56 FLOCK 4H-33
NORAD 66736
AIGLONSAT-1
NORAD 68437
0.732 12.70 5.1e-06
2026-10-12 13:14:16 FLOCK 4H-33
NORAD 66736
AIGLONSAT-1
NORAD 68437
4.276 12.73 1.5e-07
2026-10-12 14:01:36 FLOCK 4H-3
NORAD 66706
AIGLONSAT-1
NORAD 68437
1.247 12.67 1.8e-06
2026-10-12 14:09:59 STARLINK-5507
NORAD 55638
AIGLONSAT-1
NORAD 68437
3.138 13.95 6.8e-06
2026-10-12 16:24:09 AIGLONSAT-1
NORAD 68437
OBJECT J
NORAD 51832
4.991 11.77 1.2e-07
2026-10-13 22:09:38 OBJECT C
NORAD 67748
AIGLONSAT-1
NORAD 68437
4.441 15.05 8.1e-08
2026-10-13 22:24:16 TRANSPORTER-16 OBJECT L
NORAD 68426
AIGLONSAT-1
NORAD 68437
2.215 0.02 8.9e-07
2026-10-13 23:11:10 TRANSPORTER-16 OBJECT L
NORAD 68426
AIGLONSAT-1
NORAD 68437
1.138 0.02 3.4e-06
2026-10-14 02:58:39 WORLDVIEW-1 (WV-1)
NORAD 32060
AIGLONSAT-1
NORAD 68437
0.433 14.90 9.1e-06
2026-10-14 20:26:17 LUCA (RS90S)
NORAD 67287
AIGLONSAT-1
NORAD 68437
4.026 12.82 1.7e-07
2026-10-15 08:16:00 ZIYUAN 3-02 (ZY 3-02)
NORAD 41556
AIGLONSAT-1
NORAD 68437
3.900 12.79 1.8e-07
2026-10-15 10:40:14 HAWK-12C
NORAD 64621
AIGLONSAT-1
NORAD 68437
4.807 5.56 1.8e-07
2026-10-15 12:12:38 SPEQTRE
NORAD 66769
AIGLONSAT-1
NORAD 68437
4.446 12.71 1.4e-07
2026-10-15 13:35:45 YAOGAN-39 02A
NORAD 57886
AIGLONSAT-1
NORAD 68437
3.528 10.94 2.6e-07
2026-10-16 03:59:29 CARTOSAT-3
NORAD 44804
AIGLONSAT-1
NORAD 68437
3.218 11.79 2.9e-07
2026-10-16 04:46:26 ZIYUAN 3-03 (ZY 3-03)
NORAD 45939
AIGLONSAT-1
NORAD 68437
4.608 12.32 1.3e-07
2026-10-16 07:08:08 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
4.413 12.74 1.4e-07
2026-10-16 07:55:27 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
2.043 12.70 6.5e-07
2026-10-16 09:30:07 MICE-1
NORAD 66684
AIGLONSAT-1
NORAD 68437
4.567 12.66 1.3e-07
2026-10-16 17:17:33 CONNECTA IOT-12
NORAD 64553
AIGLONSAT-1
NORAD 68437
4.270 14.78 9.7e-08
2026-10-16 22:54:48 AIGLONSAT-1
NORAD 68437
FENGYUN 1C DEB
NORAD 30882
4.057 11.93 1.8e-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