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 24819U 26065.78895669 +.00000000 +00000-0 +00000-0 0 00004
2 24819 11.3392 38.5605 0007568 35.3554 341.7781 0.99502205 06
| Epoch (UTC): | 06 March 2026 18:56:05 |
| Eccentricity: | 0.0007568 |
| inclination: | 11.3392° |
| perigee height: | 35972 km |
| apogee height: | 36036 km |
| right ascension of ascending node: | 38.5605° |
| argument of perigee: | 35.3554° |
| revolutions per day: | 0.99502205 |
| mean anomaly at epoch: | 341.7781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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