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 45434U 26145.40517226 +.00000000 +00000-0 -35142-4 0 00008
2 45434 87.8912 25.5988 0001813 69.1986 290.9336 13.11418753 02
| Epoch (UTC): | 25 May 2026 09:43:26 |
| Eccentricity: | 0.0001813 |
| inclination: | 87.8912° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5988° |
| argument of perigee: | 69.1986° |
| revolutions per day: | 13.11418753 |
| mean anomaly at epoch: | 290.9336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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