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 62381U 26144.79797014 +.00000000 +00000-0 +20432-3 0 00008
2 62381 45.0051 57.2547 0003715 76.8953 283.2346 15.29973254 06
| Epoch (UTC): | 24 May 2026 19:09:04 |
| Eccentricity: | 0.0003715 |
| inclination: | 45.0051° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 57.2547° |
| argument of perigee: | 76.8953° |
| revolutions per day: | 15.29973254 |
| mean anomaly at epoch: | 283.2346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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