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 58369U 26145.64624865 +.00000000 +00000-0 -27109-3 0 00006
2 58369 42.9976 276.2712 0001084 266.8240 93.2487 15.27599938 09
| Epoch (UTC): | 25 May 2026 15:30:35 |
| Eccentricity: | 0.0001084 |
| inclination: | 42.9976° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.2712° |
| argument of perigee: | 266.8240° |
| revolutions per day: | 15.27599938 |
| mean anomaly at epoch: | 93.2487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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