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PHI-1

In orbit NORAD 66775 RYNA-2795-1118-6092-9017

Time in UTC

08:36

Next pass · Чукотка · 69°

15.10 08:36

Scheduled · Чукотка

1062

Observations over 30 days

83%

Successful observations

100k

Frames, latest 2026-10-15 07:27 UTC

Mission information
Spacecraft name
PHI-1
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-11-28 18:44:30
Separation time
2025-11-28 19:39:28
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
493.04 km
Apogee
497.29 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6873.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66775U 25276DP  26287.16632246  .00006142  00000-0  26779-3 0  9995
2 66775 97.4020 359.1382 0003089 96.4832 263.6757 15.22533166 48549
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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
2026-10-16 15:53:36 ION SCV-017
NORAD 63230
PHI 1
NORAD 66775
4.993 15.09 6.3e-08
2026-10-16 19:24:57 PHI 1
NORAD 66775
COSMOS 2251 DEB
NORAD 33765
4.593 13.05 1.2e-07
2026-10-16 21:50:37 PHI 1
NORAD 66775
OBJECT H
NORAD 67255
2.165 1.38 9.4e-07
2026-10-17 08:50:03 TRANSPORTER-15 OBJECT DM
NORAD 66773
PHI 1
NORAD 66775
3.075 0.01 4.6e-07
2026-10-17 21:30:34 ICEYE-X2
NORAD 43800
PHI 1
NORAD 66775
4.219 2.65 2.4e-07
2026-10-18 00:24:28 PHI 1
NORAD 66775
HULIANWANG JISHU SHIYAN 9D
NORAD 68834
4.891 14.54 8.0e-08
2026-10-18 02:13:41 MACSAT (FINCH 1)
NORAD 58024
PHI 1
NORAD 66775
4.666 1.41 2.0e-07
2026-10-18 20:36:49 YAOGAN-43 01C
NORAD 60460
PHI 1
NORAD 66775
0.778 11.87 5.0e-06
2026-10-18 20:42:26 PHI 1
NORAD 66775
DRISHTI
NORAD 69010
2.519 15.10 2.5e-07
2026-10-18 22:07:10 STARLINK-5613
NORAD 55752
PHI 1
NORAD 66775
4.792 5.79 5.4e-06
2026-10-18 22:47:26 PHI 1
NORAD 66775
BESSA
NORAD 68836
3.113 12.71 2.8e-07
2026-10-18 23:32:02 OBJECT B
NORAD 66054
PHI 1
NORAD 66775
3.894 0.47 2.9e-07
2026-10-19 03:53:14 HERMES-6
NORAD 63489
PHI 1
NORAD 66775
4.790 15.11 6.8e-08
2026-10-20 01:06:35 YAOGAN-36 05B
NORAD 57454
PHI 1
NORAD 66775
2.439 8.09 6.4e-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