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 62574U 26145.19705414 +.00000000 +00000-0 +48515-3 0 00002
2 62574 42.9998 220.4849 0001040 277.9795 82.0939 15.27576427 04
| Epoch (UTC): | 25 May 2026 04:43:45 |
| Eccentricity: | 0.0001040 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 220.4849° |
| argument of perigee: | 277.9795° |
| revolutions per day: | 15.27576427 |
| mean anomaly at epoch: | 82.0939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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