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 58002U 26145.61486634 +.00000000 +00000-0 +73163-4 0 00008
2 58002 43.0045 352.3871 0001047 262.9861 97.0871 15.27585380 04
| Epoch (UTC): | 25 May 2026 14:45:24 |
| Eccentricity: | 0.0001047 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.3871° |
| argument of perigee: | 262.9861° |
| revolutions per day: | 15.27585380 |
| mean anomaly at epoch: | 97.0871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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