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 65901U 26145.05142273 +.00000000 +00000-0 +69449-3 0 00001
2 65901 53.1603 16.7910 0001026 74.2284 285.8830 15.30215452 03
| Epoch (UTC): | 25 May 2026 01:14:02 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.7910° |
| argument of perigee: | 74.2284° |
| revolutions per day: | 15.30215452 |
| mean anomaly at epoch: | 285.8830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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