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 58900U 26145.51765007 +.00000000 +00000-0 +39606-3 0 00001
2 58900 97.4137 355.2480 0009450 185.0445 175.0707 15.38888551 06
| Epoch (UTC): | 25 May 2026 12:25:24 |
| Eccentricity: | 0.0009450 |
| inclination: | 97.4137° |
| perigee height: | 443 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 355.2480° |
| argument of perigee: | 185.0445° |
| revolutions per day: | 15.38888551 |
| mean anomaly at epoch: | 175.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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