View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65250U 26145.12586544 +.00000000 +00000-0 +31562-3 0 00004
2 65250 97.4470 188.0023 0002325 133.5075 226.6345 15.05657557 03
| Epoch (UTC): | 25 May 2026 03:01:14 |
| Eccentricity: | 0.0002325 |
| inclination: | 97.4470° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.0023° |
| argument of perigee: | 133.5075° |
| revolutions per day: | 15.05657557 |
| mean anomaly at epoch: | 226.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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