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 24971U 26066.71396450 +.00000000 +00000-0 +10475-3 0 00001
2 24971 98.8395 58.6018 0052360 165.5448 194.7248 14.35468913 03
| Epoch (UTC): | 07 March 2026 17:08:06 |
| Eccentricity: | 0.0052360 |
| inclination: | 98.8395° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 58.6018° |
| argument of perigee: | 165.5448° |
| revolutions per day: | 14.35468913 |
| mean anomaly at epoch: | 194.7248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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