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 00058U 26047.03528490 +.00000000 +00000-0 +27798-4 0 00003
2 00058 28.3296 34.4751 0164752 284.5715 73.6612 13.46424433 05
| Epoch (UTC): | 16 February 2026 00:50:48 |
| Eccentricity: | 0.0164752 |
| inclination: | 28.3296° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 34.4751° |
| argument of perigee: | 284.5715° |
| revolutions per day: | 13.46424433 |
| mean anomaly at epoch: | 73.6612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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