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 58693U 26145.57573950 +.00000000 +00000-0 +68373-4 0 00004
2 58693 49.9993 67.0687 0001303 16.5243 343.5677 13.41458857 09
| Epoch (UTC): | 25 May 2026 13:49:03 |
| Eccentricity: | 0.0001303 |
| inclination: | 49.9993° |
| perigee height: | 1103 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 67.0687° |
| argument of perigee: | 16.5243° |
| revolutions per day: | 13.41458857 |
| mean anomaly at epoch: | 343.5677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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