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 62252U 26145.60264397 +.00000000 +00000-0 +11248-3 0 00004
2 62252 89.0099 24.7679 0015351 85.8269 274.4636 13.51009745 09
| Epoch (UTC): | 25 May 2026 14:27:48 |
| Eccentricity: | 0.0015351 |
| inclination: | 89.0099° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 24.7679° |
| argument of perigee: | 85.8269° |
| revolutions per day: | 13.51009745 |
| mean anomaly at epoch: | 274.4636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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