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 24834U 26106.27878823 +.00000000 +00000-0 +00000-0 0 00004
2 24834 15.6230 6.5333 0104148 237.1790 350.8077 0.96050955 06
| Epoch (UTC): | 16 April 2026 06:41:27 |
| Eccentricity: | 0.0104148 |
| inclination: | 15.6230° |
| perigee height: | 36561 km |
| apogee height: | 37465 km |
| right ascension of ascending node: | 6.5333° |
| argument of perigee: | 237.1790° |
| revolutions per day: | 0.96050955 |
| mean anomaly at epoch: | 350.8077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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