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 65502U 26145.65572578 +.00000000 +00000-0 +36748-3 0 00005
2 65502 53.1587 272.8130 0002243 97.7164 262.4093 15.34399361 07
| Epoch (UTC): | 25 May 2026 15:44:14 |
| Eccentricity: | 0.0002243 |
| inclination: | 53.1587° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 272.8130° |
| argument of perigee: | 97.7164° |
| revolutions per day: | 15.34399361 |
| mean anomaly at epoch: | 262.4093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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