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 26075.84513270 +.00000000 +00000-0 +86759-4 0 00005
2 24971 98.8401 67.9561 0052841 138.8978 221.6206 14.35474246 02
| Epoch (UTC): | 16 March 2026 20:16:59 |
| Eccentricity: | 0.0052841 |
| inclination: | 98.8401° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 67.9561° |
| argument of perigee: | 138.8978° |
| revolutions per day: | 14.35474246 |
| mean anomaly at epoch: | 221.6206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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