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 26158.75398006 +.00000000 +00000-0 +98419-4 0 00003
2 24298 70.7634 344.6138 0014653 351.2685 8.8177 14.12442838 00
| Epoch (UTC): | 07 June 2026 18:05:43 |
| Eccentricity: | 0.0014653 |
| inclination: | 70.7634° |
| perigee height: | 840 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 344.6138° |
| argument of perigee: | 351.2685° |
| revolutions per day: | 14.12442838 |
| mean anomaly at epoch: | 8.8177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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