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 29275U 26161.38068517 +.00000000 +00000-0 +12148-2 0 00000
2 29275 6.0412 93.4937 6979432 151.3372 277.8355 2.67388927 06
| Epoch (UTC): | 10 June 2026 09:08:11 |
| Eccentricity: | 0.6979432 |
| inclination: | 6.0412° |
| perigee height: | 245 km |
| apogee height: | 30852 km |
| right ascension of ascending node: | 93.4937° |
| argument of perigee: | 151.3372° |
| revolutions per day: | 2.67388927 |
| mean anomaly at epoch: | 277.8355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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