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 62812U 26145.19347977 +.00000000 +00000-0 +19206-3 0 00008
2 62812 53.1604 314.1005 0000988 90.2258 269.8856 15.30183011 02
| Epoch (UTC): | 25 May 2026 04:38:36 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.1005° |
| argument of perigee: | 90.2258° |
| revolutions per day: | 15.30183011 |
| mean anomaly at epoch: | 269.8856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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