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 26039.98756605 +.00000000 +00000-0 +68821-4 0 00003
2 24298 70.7565 235.9911 0017512 188.2753 171.8080 14.12407337 04
| Epoch (UTC): | 08 February 2026 23:42:05 |
| Eccentricity: | 0.0017512 |
| inclination: | 70.7565° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 235.9911° |
| argument of perigee: | 188.2753° |
| revolutions per day: | 14.12407337 |
| mean anomaly at epoch: | 171.8080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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