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 58295U 26145.59245286 +.00000000 +00000-0 +19947-3 0 00004
2 58295 97.3988 241.7689 0009020 150.4524 209.7243 15.57900705 00
| Epoch (UTC): | 25 May 2026 14:13:07 |
| Eccentricity: | 0.0009020 |
| inclination: | 97.3988° |
| perigee height: | 388 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 241.7689° |
| argument of perigee: | 150.4524° |
| revolutions per day: | 15.57900705 |
| mean anomaly at epoch: | 209.7243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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