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 58918U 26145.65153830 +.00000000 +00000-0 +31898-3 0 00005
2 58918 97.3078 212.6897 0016971 209.4692 150.5589 15.21376632 07
| Epoch (UTC): | 25 May 2026 15:38:12 |
| Eccentricity: | 0.0016971 |
| inclination: | 97.3078° |
| perigee height: | 490 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 212.6897° |
| argument of perigee: | 209.4692° |
| revolutions per day: | 15.21376632 |
| mean anomaly at epoch: | 150.5589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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