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 26128.15971375 +.00000000 +00000-0 +92642-4 0 00002
2 24298 70.7627 49.3643 0012719 43.3527 316.8590 14.12431860 01
| Epoch (UTC): | 08 May 2026 03:49:59 |
| Eccentricity: | 0.0012719 |
| inclination: | 70.7627° |
| perigee height: | 842 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 49.3643° |
| argument of perigee: | 43.3527° |
| revolutions per day: | 14.12431860 |
| mean anomaly at epoch: | 316.8590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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