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Foresail-1p

In orbit NORAD 66778 VVCO-9182-2144-7766-7316 Finland

Time in UTC

08:21

Next pass · Чукотка · 56°

700

Observations over 30 days

55%

Successful observations

74k

Frames, latest 2026-10-15 07:06 UTC

Mission information
Spacecraft name
Foresail-1p
Other names
OH2F1S, FS1p, Foresail-1 Prime
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 18:18:00
Separation time
2025-12-09 09:18:59
Last observers
Observer
Time of receipt
2026-10-15 07:06:17 UTC
2026-10-15 05:30:02 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.68 km
Apogee
506.60 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6882.3 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 66778U 25276DS  26287.15309216  .00005383  00000-0  25627-3 0  9992
2 66778 97.4087 358.2388 0003571 70.8089 289.3532 15.19558386 48461
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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
2026-10-15 09:04:29 FORESAIL-1 PRIME
NORAD 66778
COSMOS 397 DEB
NORAD 5011
4.117 15.07 9.8e-08
2026-10-15 12:37:57 SPACEMOBILE-001
NORAD 61047
FORESAIL-1 PRIME
NORAD 66778
4.229 12.84 1.5e-07
2026-10-15 13:04:48 FORESAIL-1 PRIME
NORAD 66778
BREEZE-M DEB
NORAD 32030
4.215 14.60 1.4e-07
2026-10-16 10:15:41 FORESAIL-1 PRIME
NORAD 66778
THORAD AGENA D DEB
NORAD 4157
4.464 15.11 7.8e-08
2026-10-16 20:56:58 STARLINK-6065
NORAD 56812
FORESAIL-1 PRIME
NORAD 66778
3.680 13.48 5.4e-06
2026-10-17 07:07:09 ALISIO-1
NORAD 58562
FORESAIL-1 PRIME
NORAD 66778
2.583 0.22 6.6e-07
2026-10-17 08:43:16 AAC-HSI-SAT3
NORAD 58848
FORESAIL-1 PRIME
NORAD 66778
3.977 2.06 2.8e-07
2026-10-17 10:04:44 STARLINK-1184
NORAD 45098
FORESAIL-1 PRIME
NORAD 66778
3.409 7.72 1.0e-05
2026-10-17 11:51:19 FORESAIL-1 PRIME
NORAD 66778
RASSVET-3 6
NORAD 68365
2.831 12.60 3.4e-07
2026-10-20 15:42:56 FORESAIL-1 PRIME
NORAD 66778
RASSVET-3 3
NORAD 68362
3.046 13.08 2.8e-07
2026-10-20 15:53:19 FORESAIL-1 PRIME
NORAD 66778
TIROS 8 DEB
NORAD 19396
4.856 13.65 9.9e-08
2026-10-20 18:05:05 BLACKJACK ACES-1
NORAD 56956
FORESAIL-1 PRIME
NORAD 66778
3.664 8.13 2.8e-07
2026-10-20 18:52:31 BLACKJACK ACES-1
NORAD 56956
FORESAIL-1 PRIME
NORAD 66778
0.826 8.11 5.6e-06
2026-10-20 20:29:02 CENTAURI-1
NORAD 43809
FORESAIL-1 PRIME
NORAD 66778
3.282 2.87 4.0e-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