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 63862U 26145.01739141 +.00000000 +00000-0 +51163-3 0 00001
2 63862 43.0025 6.9557 0001601 283.6076 76.4598 15.27595341 04
| Epoch (UTC): | 25 May 2026 00:25:02 |
| Eccentricity: | 0.0001601 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.9557° |
| argument of perigee: | 283.6076° |
| revolutions per day: | 15.27595341 |
| mean anomaly at epoch: | 76.4598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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