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 24307U 26065.48900971 +.00000000 +00000-0 +00000-0 0 00006
2 24307 9.6248 54.9655 0006080 294.4303 243.3921 0.99978318 08
| Epoch (UTC): | 06 March 2026 11:44:10 |
| Eccentricity: | 0.0006080 |
| inclination: | 9.6248° |
| perigee height: | 35843 km |
| apogee height: | 35895 km |
| right ascension of ascending node: | 54.9655° |
| argument of perigee: | 294.4303° |
| revolutions per day: | 0.99978318 |
| mean anomaly at epoch: | 243.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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