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 29494U 26145.56370833 +.00000000 +00000-0 +00000-0 0 00004
2 29494 2.3647 81.1646 0004862 354.9190 268.8038 1.00271573 00
| Epoch (UTC): | 25 May 2026 13:31:44 |
| Eccentricity: | 0.0004862 |
| inclination: | 2.3647° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 81.1646° |
| argument of perigee: | 354.9190° |
| revolutions per day: | 1.00271573 |
| mean anomaly at epoch: | 268.8038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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