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 65855U 26145.42515539 +.00000000 +00000-0 +87636-3 0 00007
2 65855 53.1601 297.7841 0001118 106.3971 253.7153 15.30214105 01
| Epoch (UTC): | 25 May 2026 10:12:13 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.7841° |
| argument of perigee: | 106.3971° |
| revolutions per day: | 15.30214105 |
| mean anomaly at epoch: | 253.7153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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