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 59213U 26145.44323284 +.00000000 +00000-0 +24062-4 0 00009
2 59213 53.1606 157.9505 0001148 82.4310 277.6823 15.34391150 04
| Epoch (UTC): | 25 May 2026 10:38:15 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.9505° |
| argument of perigee: | 82.4310° |
| revolutions per day: | 15.34391150 |
| mean anomaly at epoch: | 277.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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