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 62379U 26145.12486936 +.00000000 +00000-0 +20845-3 0 00009
2 62379 45.0164 56.0775 0002838 94.1672 265.9536 15.29977550 05
| Epoch (UTC): | 25 May 2026 02:59:48 |
| Eccentricity: | 0.0002838 |
| inclination: | 45.0164° |
| perigee height: | 474 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 56.0775° |
| argument of perigee: | 94.1672° |
| revolutions per day: | 15.29977550 |
| mean anomaly at epoch: | 265.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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