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 59067U 26145.59386051 +.00000000 +00000-0 +29844-3 0 00005
2 59067 95.3917 219.4708 0146861 48.2683 313.0993 14.93143721 04
| Epoch (UTC): | 25 May 2026 14:15:09 |
| Eccentricity: | 0.0146861 |
| inclination: | 95.3917° |
| perigee height: | 486 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 219.4708° |
| argument of perigee: | 48.2683° |
| revolutions per day: | 14.93143721 |
| mean anomaly at epoch: | 313.0993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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