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 62367U 26145.49537584 +.00000000 +00000-0 +12069-3 0 00001
2 62367 44.9856 62.6840 0010523 261.9861 97.9778 13.99184157 07
| Epoch (UTC): | 25 May 2026 11:53:20 |
| Eccentricity: | 0.0010523 |
| inclination: | 44.9856° |
| perigee height: | 889 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 62.6840° |
| argument of perigee: | 261.9861° |
| revolutions per day: | 13.99184157 |
| mean anomaly at epoch: | 97.9778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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