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 62756U 26145.60365150 +.00000000 +00000-0 +12405-2 0 00007
2 62756 42.9991 248.0839 0001612 279.5770 80.4917 15.76434968 05
| Epoch (UTC): | 25 May 2026 14:29:15 |
| Eccentricity: | 0.0001612 |
| inclination: | 42.9991° |
| perigee height: | 339 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 248.0839° |
| argument of perigee: | 279.5770° |
| revolutions per day: | 15.76434968 |
| mean anomaly at epoch: | 80.4917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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