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 66058U 26145.53678039 +.00000000 +00000-0 +44670-3 0 00001
2 66058 53.1606 244.9798 0000551 16.5939 343.5082 15.34392991 06
| Epoch (UTC): | 25 May 2026 12:52:57 |
| Eccentricity: | 0.0000551 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.9798° |
| argument of perigee: | 16.5939° |
| revolutions per day: | 15.34392991 |
| mean anomaly at epoch: | 343.5082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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