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 62412U 26145.22452530 +.00000000 +00000-0 +15480-2 0 00009
2 62412 42.9898 57.6357 0014321 226.2952 133.6742 16.05146906 03
| Epoch (UTC): | 25 May 2026 05:23:18 |
| Eccentricity: | 0.0014321 |
| inclination: | 42.9898° |
| perigee height: | 251 km |
| apogee height: | 270 km |
| right ascension of ascending node: | 57.6357° |
| argument of perigee: | 226.2952° |
| revolutions per day: | 16.05146906 |
| mean anomaly at epoch: | 133.6742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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