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 62129U 26145.03628275 +.00000000 +00000-0 +66526-3 0 00002
2 62129 43.0025 61.6886 0002278 256.9887 103.0711 15.27599315 05
| Epoch (UTC): | 25 May 2026 00:52:14 |
| Eccentricity: | 0.0002278 |
| inclination: | 43.0025° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 61.6886° |
| argument of perigee: | 256.9887° |
| revolutions per day: | 15.27599315 |
| mean anomaly at epoch: | 103.0711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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