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 58794U 26145.20144125 +.00000000 +00000-0 -31320-4 0 00007
2 58794 42.9997 93.4676 0001810 178.1833 181.9025 15.27572343 06
| Epoch (UTC): | 25 May 2026 04:50:04 |
| Eccentricity: | 0.0001810 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.4676° |
| argument of perigee: | 178.1833° |
| revolutions per day: | 15.27572343 |
| mean anomaly at epoch: | 181.9025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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