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 24278U 26145.31709001 +.00000000 +00000-0 +25710-4 0 00004
2 24278 98.5263 357.3196 0350299 155.6468 206.1682 13.53273146 05
| Epoch (UTC): | 25 May 2026 07:36:36 |
| Eccentricity: | 0.0350299 |
| inclination: | 98.5263° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 357.3196° |
| argument of perigee: | 155.6468° |
| revolutions per day: | 13.53273146 |
| mean anomaly at epoch: | 206.1682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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