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 26039.56263610 +.00000000 +00000-0 +68150-4 0 00001
2 24298 70.7565 236.8906 0017545 188.8072 171.2743 14.12407240 07
| Epoch (UTC): | 08 February 2026 13:30:11 |
| Eccentricity: | 0.0017545 |
| inclination: | 70.7565° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 236.8906° |
| argument of perigee: | 188.8072° |
| revolutions per day: | 14.12407240 |
| mean anomaly at epoch: | 171.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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