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 62974U 26145.57291459 +.00000000 +00000-0 +46510-4 0 00001
2 62974 50.0043 316.7312 0001116 97.3004 262.7995 13.29324024 07
| Epoch (UTC): | 25 May 2026 13:44:59 |
| Eccentricity: | 0.0001116 |
| inclination: | 50.0043° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 316.7312° |
| argument of perigee: | 97.3004° |
| revolutions per day: | 13.29324024 |
| mean anomaly at epoch: | 262.7995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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