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 58334U 26145.60697515 +.00000000 +00000-0 +53047-3 0 00005
2 58334 97.3959 237.7353 0005823 187.4736 172.6432 15.55852589 09
| Epoch (UTC): | 25 May 2026 14:34:02 |
| Eccentricity: | 0.0005823 |
| inclination: | 97.3959° |
| perigee height: | 396 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 237.7353° |
| argument of perigee: | 187.4736° |
| revolutions per day: | 15.55852589 |
| mean anomaly at epoch: | 172.6432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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