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 58395U 26145.32129580 +.00000000 +00000-0 +12221-3 0 00002
2 58395 53.1606 4.5233 0001262 96.3550 263.7597 15.34378766 08
| Epoch (UTC): | 25 May 2026 07:42:39 |
| Eccentricity: | 0.0001262 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 4.5233° |
| argument of perigee: | 96.3550° |
| revolutions per day: | 15.34378766 |
| mean anomaly at epoch: | 263.7597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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