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 62972U 26145.53941361 +.00000000 +00000-0 +55282-4 0 00005
2 62972 50.0034 317.1828 0001291 98.2650 261.8369 13.29321793 08
| Epoch (UTC): | 25 May 2026 12:56:45 |
| Eccentricity: | 0.0001291 |
| inclination: | 50.0034° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 317.1828° |
| argument of perigee: | 98.2650° |
| revolutions per day: | 13.29321793 |
| mean anomaly at epoch: | 261.8369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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