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 62826U 26145.17213686 +.00000000 +00000-0 +21940-2 0 00007
2 62826 53.1562 313.2627 0003621 267.0572 93.0017 15.36131536 07
| Epoch (UTC): | 25 May 2026 04:07:52 |
| Eccentricity: | 0.0003621 |
| inclination: | 53.1562° |
| perigee height: | 455 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 313.2627° |
| argument of perigee: | 267.0572° |
| revolutions per day: | 15.36131536 |
| mean anomaly at epoch: | 93.0017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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