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 26039.84592272 +.00000000 +00000-0 +70148-4 0 00001
2 24298 70.7565 236.2910 0017526 188.4618 171.6208 14.12407310 05
| Epoch (UTC): | 08 February 2026 20:18:07 |
| Eccentricity: | 0.0017526 |
| inclination: | 70.7565° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 236.2910° |
| argument of perigee: | 188.4618° |
| revolutions per day: | 14.12407310 |
| mean anomaly at epoch: | 171.6208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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