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 59959U 26145.20912233 +.00000000 +00000-0 +90227-4 0 00004
2 59959 53.1606 69.9846 0001210 82.7607 277.3532 15.30201513 06
| Epoch (UTC): | 25 May 2026 05:01:08 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 69.9846° |
| argument of perigee: | 82.7607° |
| revolutions per day: | 15.30201513 |
| mean anomaly at epoch: | 277.3532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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