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 29601U 26144.48591470 +.00000000 +00000-0 +00000-0 0 00006
2 29601 54.9372 214.9460 0085625 90.6191 270.4207 2.00556865 07
| Epoch (UTC): | 24 May 2026 11:39:43 |
| Eccentricity: | 0.0085625 |
| inclination: | 54.9372° |
| perigee height: | 19955 km |
| apogee height: | 20410 km |
| right ascension of ascending node: | 214.9460° |
| argument of perigee: | 90.6191° |
| revolutions per day: | 2.00556865 |
| mean anomaly at epoch: | 270.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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