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 54871U 26145.43766122 +.00000000 +00000-0 +43072-5 0 00008
2 54871 43.0061 48.5323 0001107 264.8375 95.2351 15.27575320 02
| Epoch (UTC): | 25 May 2026 10:30:13 |
| Eccentricity: | 0.0001107 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5323° |
| argument of perigee: | 264.8375° |
| revolutions per day: | 15.27575320 |
| mean anomaly at epoch: | 95.2351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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