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 65627U 26145.47633042 +.00000000 +00000-0 +82491-3 0 00003
2 65627 53.1591 310.6809 0001118 74.7301 285.3823 15.30212171 06
| Epoch (UTC): | 25 May 2026 11:25:54 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6809° |
| argument of perigee: | 74.7301° |
| revolutions per day: | 15.30212171 |
| mean anomaly at epoch: | 285.3823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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