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 54806U 26145.25227140 +.00000000 +00000-0 +34140-4 0 00003
2 54806 53.2114 45.0065 0001153 71.4124 288.6994 15.08848347 04
| Epoch (UTC): | 25 May 2026 06:03:16 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.0065° |
| argument of perigee: | 71.4124° |
| revolutions per day: | 15.08848347 |
| mean anomaly at epoch: | 288.6994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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