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 62436U 26145.26835828 +.00000000 +00000-0 +62752-3 0 00009
2 62436 53.1613 339.5582 0001009 70.3227 289.7883 15.30208338 06
| Epoch (UTC): | 25 May 2026 06:26:26 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.5582° |
| argument of perigee: | 70.3227° |
| revolutions per day: | 15.30208338 |
| mean anomaly at epoch: | 289.7883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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