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 29967U 26088.17606727 +.00000000 +00000-0 +13117-2 0 00001
2 29967 98.8545 170.6286 0072846 347.3012 42.1291 14.24391131 09
| Epoch (UTC): | 29 March 2026 04:13:32 |
| Eccentricity: | 0.0072846 |
| inclination: | 98.8545° |
| perigee height: | 758 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 170.6286° |
| argument of perigee: | 347.3012° |
| revolutions per day: | 14.24391131 |
| mean anomaly at epoch: | 42.1291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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