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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
492.63 km
Apogee
496.93 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6872.9 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68437U 26067X   26286.85159286  .00014756  00000-0  63603-3 0  9991
2 68437 97.4654 244.1589 0003129 41.3674 318.7799 15.22662063 29983
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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 09:05:36 HAWK-12B
NORAD 64622
AIGLONSAT-1
NORAD 68437
3.557 5.67 3.3e-07
2026-10-15 11:57:24 AIGLONSAT-1
NORAD 68437
COSMOS 2251 DEB
NORAD 36441
3.896 15.21 9.9e-08
2026-10-15 12:59:58 SPEQTRE
NORAD 66769
AIGLONSAT-1
NORAD 68437
4.103 12.68 1.6e-07
2026-10-16 02:24:17 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
4.476 12.74 1.4e-07
2026-10-16 03:11:36 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
2.261 12.70 5.3e-07
2026-10-16 07:55:43 ZIYUAN 3-03 (ZY 3-03)
NORAD 45939
AIGLONSAT-1
NORAD 68437
1.855 12.32 8.3e-07
2026-10-16 18:52:12 CONNECTA IOT-12
NORAD 64553
AIGLONSAT-1
NORAD 68437
1.996 14.78 4.4e-07
2026-10-16 20:25:45 STARLINK-5925
NORAD 55945
AIGLONSAT-1
NORAD 68437
2.160 14.93 1.1e-05
2026-10-17 04:06:00 AIGLONSAT-1
NORAD 68437
RAWHIDE-2
NORAD 68632
3.769 14.93 1.2e-07
2026-10-18 06:43:01 STARLINK-5142
NORAD 53984
AIGLONSAT-1
NORAD 68437
4.784 7.72 5.1e-06
2026-10-18 07:05:10 STARLINK-5862
NORAD 55920
AIGLONSAT-1
NORAD 68437
3.428 15.02 4.1e-06
2026-10-18 11:53:19 SUPERVIEW NEO-1 04
NORAD 63126
AIGLONSAT-1
NORAD 68437
4.022 14.70 1.1e-07
2026-10-18 12:40:38 SUPERVIEW NEO-1 04
NORAD 63126
AIGLONSAT-1
NORAD 68437
4.706 14.73 8.2e-08
2026-10-19 01:26:40 TRANSPORTER-13 OBJECT M
NORAD 63221
AIGLONSAT-1
NORAD 68437
3.083 8.38 4.0e-07
2026-10-19 03:01:17 TRANSPORTER-13 OBJECT M
NORAD 63221
AIGLONSAT-1
NORAD 68437
2.824 8.38 4.7e-07
2026-10-19 05:23:15 TRANSPORTER-13 OBJECT M
NORAD 63221
AIGLONSAT-1
NORAD 68437
3.334 8.36 3.4e-07
2026-10-19 06:57:52 TRANSPORTER-13 OBJECT M
NORAD 63221
AIGLONSAT-1
NORAD 68437
4.482 8.36 1.9e-07
2026-10-19 07:45:01 AIGLONSAT-1
NORAD 68437
QUBE-II
NORAD 69023
4.625 7.74 1.8e-07
2026-10-19 08:23:26 SUPERVIEW NEO-1 03
NORAD 63125
AIGLONSAT-1
NORAD 68437
3.583 14.70 1.4e-07
2026-10-19 08:32:22 AIGLONSAT-1
NORAD 68437
QUBE-II
NORAD 69023
3.409 7.72 3.3e-07
2026-10-19 09:10:46 SUPERVIEW NEO-1 03
NORAD 63125
AIGLONSAT-1
NORAD 68437
4.367 14.73 9.5e-08

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