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 62451U 26145.55072411 +.00000000 +00000-0 +66419-3 0 00003
2 62451 53.1593 338.4711 0001141 80.0095 280.1035 15.30203067 08
| Epoch (UTC): | 25 May 2026 13:13:02 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.4711° |
| argument of perigee: | 80.0095° |
| revolutions per day: | 15.30203067 |
| mean anomaly at epoch: | 280.1035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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