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 62971U 26145.60629569 +.00000000 +00000-0 +63178-4 0 00008
2 62971 50.0017 316.8139 0001328 99.4901 260.6122 13.29321215 05
| Epoch (UTC): | 25 May 2026 14:33:03 |
| Eccentricity: | 0.0001328 |
| inclination: | 50.0017° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 316.8139° |
| argument of perigee: | 99.4901° |
| revolutions per day: | 13.29321215 |
| mean anomaly at epoch: | 260.6122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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