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 66802U 26145.43084808 +.00000000 +00000-0 +46225-3 0 00000
2 66802 43.0025 41.1442 0001265 267.2467 92.8240 15.27589592 00
| Epoch (UTC): | 25 May 2026 10:20:25 |
| Eccentricity: | 0.0001265 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.1442° |
| argument of perigee: | 267.2467° |
| revolutions per day: | 15.27589592 |
| mean anomaly at epoch: | 92.8240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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