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 26044.73261502 +.00000000 +00000-0 +81803-4 0 00004
2 24298 70.7568 225.9463 0017116 181.9487 178.1568 14.12408773 08
| Epoch (UTC): | 13 February 2026 17:34:57 |
| Eccentricity: | 0.0017116 |
| inclination: | 70.7568° |
| perigee height: | 839 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 225.9463° |
| argument of perigee: | 181.9487° |
| revolutions per day: | 14.12408773 |
| mean anomaly at epoch: | 178.1568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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