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 29049U 26088.05648169 +.00000000 +00000-0 +18742-3 0 00005
2 29049 72.0189 207.7967 0034271 343.7286 16.2749 14.31340115 03
| Epoch (UTC): | 29 March 2026 01:21:20 |
| Eccentricity: | 0.0034271 |
| inclination: | 72.0189° |
| perigee height: | 763 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 207.7967° |
| argument of perigee: | 343.7286° |
| revolutions per day: | 14.31340115 |
| mean anomaly at epoch: | 16.2749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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