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PHI-DEMO

In orbit NORAD 57181 YMVX-8330-2150-0956-9275 United Arab Emirates

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

0

Observations all time

Mission information
Spacecraft name
PHI-DEMO
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
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2023-06-27 11:34:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
506.48 km
Apogee
529.27 km
Inclination
97.5°
Period
95.0 min
Semi-major axis
6896.0 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 57181U 23091R   26283.56410826  .00002716  00000-0  14845-3 0  9991
2 57181 97.4933 335.9414 0016530 98.2125 262.0983 15.15027769181159
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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 08:59:26 OBJECT R
NORAD 57181
FEMTO-1
NORAD 68419
4.205 11.15 1.8e-07
2026-10-11 19:39:01 STARLINK-4620
NORAD 53674
OBJECT R
NORAD 57181
4.624 15.08 2.2e-06
2026-10-11 23:15:24 OBJECT R
NORAD 57181
SPOQC
NORAD 68423
3.929 11.16 2.1e-07
2026-10-11 23:36:39 STARLINK-4620
NORAD 53674
OBJECT R
NORAD 57181
4.536 15.08 2.3e-06
2026-10-12 01:11:43 STARLINK-4620
NORAD 53674
OBJECT R
NORAD 57181
2.962 15.08 5.4e-06
2026-10-13 07:43:04 OBJECT R
NORAD 57181
OBJECT T
NORAD 43775
2.219 1.54 8.9e-07
2026-10-13 16:49:54 AAC-HSI-SAT1
NORAD 56225
OBJECT R
NORAD 57181
4.034 15.07 9.6e-08
2026-10-14 11:08:55 STARLINK-3121
NORAD 49428
OBJECT R
NORAD 57181
4.025 6.13 7.6e-06
2026-10-15 00:07:22 OBJECT R
NORAD 57181
CZ-6A DEB
NORAD 60704
1.186 9.12 2.6e-06
2026-10-15 23:46:39 OBJECT R
NORAD 57181
THORAD AGENA D DEB
NORAD 4157
3.187 14.82 1.7e-07
2026-10-16 12:05:23 OBJECT R
NORAD 57181
COSMOS 2251 DEB
NORAD 38220
4.897 15.14 6.3e-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