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 54742U 26145.56613501 +.00000000 +00000-0 +00000-0 0 00000
2 54742 0.0088 244.3225 0002721 188.1489 285.4864 1.00271854 08
| Epoch (UTC): | 25 May 2026 13:35:14 |
| Eccentricity: | 0.0002721 |
| inclination: | 0.0088° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 244.3225° |
| argument of perigee: | 188.1489° |
| revolutions per day: | 1.00271854 |
| mean anomaly at epoch: | 285.4864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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