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 62916U 26145.60056156 +.00000000 +00000-0 +20031-2 0 00002
2 62916 43.0001 244.4757 0001548 303.3333 56.7386 15.70871598 09
| Epoch (UTC): | 25 May 2026 14:24:48 |
| Eccentricity: | 0.0001548 |
| inclination: | 43.0001° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 244.4757° |
| argument of perigee: | 303.3333° |
| revolutions per day: | 15.70871598 |
| mean anomaly at epoch: | 56.7386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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