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 62798U 26145.58359510 +.00000000 +00000-0 +12095-3 0 00009
2 62798 88.9730 86.1015 0013033 225.5214 134.4873 13.51012245 05
| Epoch (UTC): | 25 May 2026 14:00:22 |
| Eccentricity: | 0.0013033 |
| inclination: | 88.9730° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.1015° |
| argument of perigee: | 225.5214° |
| revolutions per day: | 13.51012245 |
| mean anomaly at epoch: | 134.4873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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