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PTD-4, PT4F1N

In orbit NORAD 60565 UOLM-4510-8859-5501-3189

Time in UTC

05:23

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 22°

141

Observations over 30 days

30%

Successful observations

594k

Frames, latest 2026-10-10 10:34 UTC

Mission information
Spacecraft name
PTD-4, PT4F1N
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2024-08-16 18:56:00
Separation time
2024-08-16 21:29:18
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
482.14 km
Apogee
485.16 km
Inclination
97.7°
Period
94.3 min
Semi-major axis
6861.8 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 60565U 24149DB  26283.22253141  .00024641  00000-0  94843-3 0  9991
2 60565 97.6943 15.1422 0002197 17.2405 342.8907 15.26368058118349
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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 08:17:41 PTD-4 (LISA-T)
NORAD 60565
PELICAN-8
NORAD 69018
4.940 14.97 6.9e-08
2026-10-11 09:52:03 PTD-4 (LISA-T)
NORAD 60565
PELICAN-8
NORAD 69018
4.919 14.97 6.9e-08
2026-10-11 10:39:15 PTD-4 (LISA-T)
NORAD 60565
PELICAN-8
NORAD 69018
4.581 14.94 8.0e-08
2026-10-11 14:32:58 STARLINK-30568
NORAD 58051
PTD-4 (LISA-T)
NORAD 60565
4.544 13.29 3.7e-06
2026-10-11 22:26:14 STARLINK-32089
NORAD 59687
PTD-4 (LISA-T)
NORAD 60565
4.781 11.80 4.0e-06
2026-10-11 22:43:57 STARLINK-5852
NORAD 55933
PTD-4 (LISA-T)
NORAD 60565
4.868 10.22 4.4e-06
2026-10-12 03:59:06 PTD-4 (LISA-T)
NORAD 60565
M-SEL/CORTEZ
NORAD 63231
3.391 14.86 1.5e-07
2026-10-12 22:01:21 STARLINK-30946
NORAD 58450
PTD-4 (LISA-T)
NORAD 60565
4.429 13.06 4.0e-06
2026-10-13 10:37:06 STARLINK-31568
NORAD 59412
PTD-4 (LISA-T)
NORAD 60565
4.391 12.53 4.4e-06
2026-10-14 12:46:04 VIGORIDE-3
NORAD 52760
PTD-4 (LISA-T)
NORAD 60565
0.673 6.53 8.9e-06
2026-10-14 13:20:52 STARLINK-5832
NORAD 57063
PTD-4 (LISA-T)
NORAD 60565
4.656 9.72 4.9e-06
2026-10-15 14:21:33 STARLINK-5759
NORAD 55592
PTD-4 (LISA-T)
NORAD 60565
4.255 14.36 3.4e-06
2026-10-15 17:40:27 STARLINK-31002
NORAD 58495
PTD-4 (LISA-T)
NORAD 60565
4.382 12.91 4.2e-06
2026-10-15 19:07:23 STARLINK-30230
NORAD 57503
PTD-4 (LISA-T)
NORAD 60565
4.387 14.30 3.2e-06
2026-10-16 01:29:58 STARLINK-31787
NORAD 59650
PTD-4 (LISA-T)
NORAD 60565
4.922 8.54 4.7e-06
2026-10-16 21:43:15 STARLINK-30909
NORAD 58363
PTD-4 (LISA-T)
NORAD 60565
4.885 14.18 2.7e-06

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