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 58419U 26145.56371720 +.00000000 +00000-0 +73804-4 0 00005
2 58419 43.0041 229.6160 0001568 263.8565 96.2108 15.27575651 02
| Epoch (UTC): | 25 May 2026 13:31:45 |
| Eccentricity: | 0.0001568 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.6160° |
| argument of perigee: | 263.8565° |
| revolutions per day: | 15.27575651 |
| mean anomaly at epoch: | 96.2108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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