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 58094U 26145.29426943 +.00000000 +00000-0 +21305-3 0 00000
2 58094 43.0013 5.0715 0001402 276.0569 84.0123 15.27585470 01
| Epoch (UTC): | 25 May 2026 07:03:44 |
| Eccentricity: | 0.0001402 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0715° |
| argument of perigee: | 276.0569° |
| revolutions per day: | 15.27585470 |
| mean anomaly at epoch: | 84.0123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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