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 62869U 26145.34575521 +.00000000 +00000-0 +35658-3 0 00004
2 62869 53.1581 133.7602 0001171 97.2138 262.8996 15.30204317 06
| Epoch (UTC): | 25 May 2026 08:17:53 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.7602° |
| argument of perigee: | 97.2138° |
| revolutions per day: | 15.30204317 |
| mean anomaly at epoch: | 262.8996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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