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 24298U 26106.70109663 +.00000000 +00000-0 +45702-4 0 00007
2 24298 70.7569 94.7826 0012636 83.2420 277.0137 14.12425460 00
| Epoch (UTC): | 16 April 2026 16:49:34 |
| Eccentricity: | 0.0012636 |
| inclination: | 70.7569° |
| perigee height: | 842 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 94.7826° |
| argument of perigee: | 83.2420° |
| revolutions per day: | 14.12425460 |
| mean anomaly at epoch: | 277.0137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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