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 65255U 26145.56614433 +.00000000 +00000-0 +10002-3 0 00002
2 65255 97.4454 188.3280 0002414 109.0442 251.1047 15.05658520 06
| Epoch (UTC): | 25 May 2026 13:35:14 |
| Eccentricity: | 0.0002414 |
| inclination: | 97.4454° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3280° |
| argument of perigee: | 109.0442° |
| revolutions per day: | 15.05658520 |
| mean anomaly at epoch: | 251.1047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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