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 29506U 26145.61919497 +.00000000 +00000-0 +11962-3 0 00001
2 29506 97.7165 174.8176 0012970 129.2256 231.0122 15.01305961 01
| Epoch (UTC): | 25 May 2026 14:51:38 |
| Eccentricity: | 0.0012970 |
| inclination: | 97.7165° |
| perigee height: | 554 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 174.8176° |
| argument of perigee: | 129.2256° |
| revolutions per day: | 15.01305961 |
| mean anomaly at epoch: | 231.0122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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