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 29517U 26107.92990155 +.00000000 +00000-0 +12548-3 0 00006
2 29517 28.2185 180.8156 4044967 156.5174 228.9041 6.89901072 02
| Epoch (UTC): | 17 April 2026 22:19:03 |
| Eccentricity: | 0.4044967 |
| inclination: | 28.2185° |
| perigee height: | 563 km |
| apogee height: | 9992 km |
| right ascension of ascending node: | 180.8156° |
| argument of perigee: | 156.5174° |
| revolutions per day: | 6.89901072 |
| mean anomaly at epoch: | 228.9041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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