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 62256U 26103.60303081 +.00000000 +00000-0 -78863-2 0 00002
2 62256 59.6796 102.9076 8010887 203.6839 74.2449 1.22066656 07
| Epoch (UTC): | 13 April 2026 14:28:21 |
| Eccentricity: | 0.8010887 |
| inclination: | 59.6796° |
| perigee height: | 978 km |
| apogee height: | 60232 km |
| right ascension of ascending node: | 102.9076° |
| argument of perigee: | 203.6839° |
| revolutions per day: | 1.22066656 |
| mean anomaly at epoch: | 74.2449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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