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 58298U 26145.61803551 +.00000000 +00000-0 +15912-3 0 00003
2 58298 97.3845 222.3469 0007671 263.3737 96.6629 15.27429046 08
| Epoch (UTC): | 25 May 2026 14:49:58 |
| Eccentricity: | 0.0007671 |
| inclination: | 97.3845° |
| perigee height: | 478 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 222.3469° |
| argument of perigee: | 263.3737° |
| revolutions per day: | 15.27429046 |
| mean anomaly at epoch: | 96.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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