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 40024U 26074.94092212 +.00000000 +00000-0 +57154-3 0 00006
2 40024 98.0836 99.2434 0005082 133.2179 226.9484 15.28382751 05
| Epoch (UTC): | 15 March 2026 22:34:55 |
| Eccentricity: | 0.0005082 |
| inclination: | 98.0836° |
| perigee height: | 477 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.2434° |
| argument of perigee: | 133.2179° |
| revolutions per day: | 15.28382751 |
| mean anomaly at epoch: | 226.9484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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