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 62882U 26145.17703920 +.00000000 +00000-0 +16740-2 0 00006
2 62882 43.0008 80.6346 0003113 269.0725 90.9786 15.70944765 06
| Epoch (UTC): | 25 May 2026 04:14:56 |
| Eccentricity: | 0.0003113 |
| inclination: | 43.0008° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 80.6346° |
| argument of perigee: | 269.0725° |
| revolutions per day: | 15.70944765 |
| mean anomaly at epoch: | 90.9786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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