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 26069.57199515 +.00000000 +00000-0 +74312-3 0 00008
2 40024 98.0846 93.4192 0004745 147.1741 212.9793 15.28163674 06
| Epoch (UTC): | 10 March 2026 13:43:40 |
| Eccentricity: | 0.0004745 |
| inclination: | 98.0846° |
| perigee height: | 478 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 93.4192° |
| argument of perigee: | 147.1741° |
| revolutions per day: | 15.28163674 |
| mean anomaly at epoch: | 212.9793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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