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 63370U 26145.58335647 +.00000000 +00000-0 +16623-2 0 00001
2 63370 53.1590 53.0273 0001235 98.7770 282.4227 15.34359323 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 53.0273° |
| argument of perigee: | 98.7770° |
| revolutions per day: | 15.34359323 |
| mean anomaly at epoch: | 282.4227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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