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 62952U 26145.51314969 +.00000000 +00000-0 +58807-3 0 00004
2 62952 53.1598 235.3312 0002025 110.1120 250.0099 15.31719812 04
| Epoch (UTC): | 25 May 2026 12:18:56 |
| Eccentricity: | 0.0002025 |
| inclination: | 53.1598° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 235.3312° |
| argument of perigee: | 110.1120° |
| revolutions per day: | 15.31719812 |
| mean anomaly at epoch: | 250.0099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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