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 26040.83742591 +.00000000 +00000-0 +73945-4 0 00001
2 24298 70.7565 234.1920 0017455 187.1709 172.9163 14.12407584 08
| Epoch (UTC): | 09 February 2026 20:05:53 |
| Eccentricity: | 0.0017455 |
| inclination: | 70.7565° |
| perigee height: | 839 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 234.1920° |
| argument of perigee: | 187.1709° |
| revolutions per day: | 14.12407584 |
| mean anomaly at epoch: | 172.9163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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