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 59215U 26145.41377286 +.00000000 +00000-0 +38406-4 0 00006
2 59215 53.1603 157.7388 0001265 94.0404 266.0743 15.34391984 01
| Epoch (UTC): | 25 May 2026 09:55:49 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.7388° |
| argument of perigee: | 94.0404° |
| revolutions per day: | 15.34391984 |
| mean anomaly at epoch: | 266.0743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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