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 59962U 26145.49042425 +.00000000 +00000-0 +56951-4 0 00002
2 59962 53.1611 68.8917 0001090 98.1308 261.9817 15.30203383 00
| Epoch (UTC): | 25 May 2026 11:46:12 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.8917° |
| argument of perigee: | 98.1308° |
| revolutions per day: | 15.30203383 |
| mean anomaly at epoch: | 261.9817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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