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 58294U 26145.51406638 +.00000000 +00000-0 +82042-3 0 00001
2 58294 97.3877 235.6796 0005479 212.7879 147.3039 15.61306362 00
| Epoch (UTC): | 25 May 2026 12:20:15 |
| Eccentricity: | 0.0005479 |
| inclination: | 97.3877° |
| perigee height: | 380 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 235.6796° |
| argument of perigee: | 212.7879° |
| revolutions per day: | 15.61306362 |
| mean anomaly at epoch: | 147.3039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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