RU | EN | ZH --:-- UTC Sign in

FORMOSAT-8A

In orbit NORAD 66666 TUSR-8011-4446-8744-0509 Taiwan

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FORMOSAT-8A
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
2025-11-28 18:44:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
558.01 km
Apogee
564.95 km
Inclination
97.7°
Period
95.9 min
Semi-major axis
6939.6 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:41 UTC
Two-line elements (TLE)
1 66666U 25276A   26285.20964892  .00001627  00000-0  13284-3 0  9992
2 66666 97.6529 357.6964 0005009 218.2228 141.8641 15.00785804 47610
Copy content
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
2026-10-13 19:00:28 FORMOSAT-8A
NORAD 66666
PEGASUS DEB
NORAD 24091
3.903 12.19 1.9e-07
2026-10-14 05:06:36 FORMOSAT-8A
NORAD 66666
STARLINK-36230
NORAD 67075
4.005 15.06 2.9e-06
2026-10-14 11:29:35 FORMOSAT-8A
NORAD 66666
STARLINK-36170
NORAD 67083
2.343 15.06 8.5e-06
2026-10-14 15:28:38 FORMOSAT-8A
NORAD 66666
FENGYUN 1C DEB
NORAD 31898
3.754 15.05 1.1e-07
2026-10-15 17:46:39 FORMOSAT-8A
NORAD 66666
PEGASUS R/B
NORAD 27652
4.634 14.04 1.0e-07
2026-10-16 03:34:04 STARLINK-5236
NORAD 55274
FORMOSAT-8A
NORAD 66666
4.998 15.04 1.9e-06
2026-10-16 12:45:00 STARLINK-5884
NORAD 55957
FORMOSAT-8A
NORAD 66666
4.621 8.71 5.3e-06
2026-10-16 23:02:04 FORMOSAT-8A
NORAD 66666
OBJECT B
NORAD 100956
3.046 3.07 4.7e-07
2026-10-17 06:31:10 FORMOSAT-8A
NORAD 66666
STARLINK-35842
NORAD 67087
3.862 15.03 3.2e-06
2026-10-17 11:00:54 FORMOSAT-8A
NORAD 66666
OBJECT U
NORAD 42843
3.609 9.63 2.7e-07
2026-10-17 19:50:11 FORMOSAT-8A
NORAD 66666
OBJECT G
NORAD 100961
4.574 3.07 2.1e-07
2026-10-18 14:36:58 STARLINK-5338
NORAD 55286
FORMOSAT-8A
NORAD 66666
3.236 15.06 4.4e-06
2026-10-18 15:02:17 FORMOSAT-8A
NORAD 66666
OBJECT H
NORAD 100962
3.346 3.07 3.9e-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