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 26105.70960704 +.00000000 +00000-0 +49664-4 0 00008
2 24298 70.7584 96.8812 0012633 85.1014 275.1548 14.12425400 01
| Epoch (UTC): | 15 April 2026 17:01:50 |
| Eccentricity: | 0.0012633 |
| inclination: | 70.7584° |
| perigee height: | 842 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 96.8812° |
| argument of perigee: | 85.1014° |
| revolutions per day: | 14.12425400 |
| mean anomaly at epoch: | 275.1548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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