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 62873U 26145.38468878 +.00000000 +00000-0 +29128-3 0 00004
2 62873 53.1571 133.2912 0000979 85.6057 274.5056 15.30202316 09
| Epoch (UTC): | 25 May 2026 09:13:57 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1571° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.2912° |
| argument of perigee: | 85.6057° |
| revolutions per day: | 15.30202316 |
| mean anomaly at epoch: | 274.5056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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