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 54828U 26145.47170402 +.00000000 +00000-0 +72603-4 0 00005
2 54828 43.0037 62.6497 0000728 223.1523 136.9272 15.27574484 02
| Epoch (UTC): | 25 May 2026 11:19:15 |
| Eccentricity: | 0.0000728 |
| inclination: | 43.0037° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.6497° |
| argument of perigee: | 223.1523° |
| revolutions per day: | 15.27574484 |
| mean anomaly at epoch: | 136.9272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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