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

Observer-1A

In orbit NORAD 58323 IXDJ-0518-1708-5570-4903 South Korea

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
Observer-1A
Other names
2023-174BV
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
2023-11-11 00:00:00
Separation time
2023-11-11 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
434.35 km
Apogee
446.78 km
Inclination
97.4°
Period
93.5 min
Semi-major axis
6818.7 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 58323U 23174BV  26283.57914558  .00012311  00000-0  30165-3 0  9999
2 58323 97.3891 8.4679 0009105 101.2461 258.9809 15.40845287162963
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
2026-10-12 14:11:28 UNISAT-7
NORAD 47945
OBSERVER-1A
NORAD 58323
3.013 15.16 1.7e-07
2026-10-12 18:54:50 STARLINK-1523
NORAD 46028
OBSERVER-1A
NORAD 58323
3.198 14.78 5.4e-06
2026-10-12 20:39:06 STARLINK-2446
NORAD 47844
OBSERVER-1A
NORAD 58323
2.491 8.90 1.8e-05
2026-10-13 22:21:50 OBSERVER-1A
NORAD 58323
KUIPER-00075
NORAD 64822
2.968 13.72 2.7e-07
2026-10-15 03:01:06 STARLINK-1047
NORAD 44752
OBSERVER-1A
NORAD 58323
1.327 14.79 3.1e-05
2026-10-15 12:02:18 STARLINK-6073
NORAD 56807
OBSERVER-1A
NORAD 58323
3.520 12.92 6.5e-06
2026-10-16 16:52:07 STARLINK-6073
NORAD 56807
OBSERVER-1A
NORAD 58323
3.009 12.65 9.2e-06
2026-10-16 19:42:53 OBSERVER-1A
NORAD 58323
TRANSPORTER-11 OBJECT AU
NORAD 60510
2.769 0.01 5.3e-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