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 62785U 26145.45587235 +.00000000 +00000-0 +14269-3 0 00003
2 62785 88.9734 86.2315 0015168 232.1299 127.8480 13.51012744 01
| Epoch (UTC): | 25 May 2026 10:56:27 |
| Eccentricity: | 0.0015168 |
| inclination: | 88.9734° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 86.2315° |
| argument of perigee: | 232.1299° |
| revolutions per day: | 13.51012744 |
| mean anomaly at epoch: | 127.8480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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