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 29045U 26145.60987948 +.00000000 +00000-0 +00000-0 0 00002
2 29045 1.0531 84.4573 0001920 345.2974 165.0541 1.00272451 03
| Epoch (UTC): | 25 May 2026 14:38:13 |
| Eccentricity: | 0.0001920 |
| inclination: | 1.0531° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 84.4573° |
| argument of perigee: | 345.2974° |
| revolutions per day: | 1.00272451 |
| mean anomaly at epoch: | 165.0541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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