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 58323U 26145.65563793 +.00000000 +00000-0 +30077-3 0 00006
2 58323 97.3940 229.2485 0006956 226.4564 133.6104 15.38063624 08
| Epoch (UTC): | 25 May 2026 15:44:07 |
| Eccentricity: | 0.0006956 |
| inclination: | 97.3940° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 229.2485° |
| argument of perigee: | 226.4564° |
| revolutions per day: | 15.38063624 |
| mean anomaly at epoch: | 133.6104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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