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 57954U 26145.34282905 +.00000000 +00000-0 +47381-4 0 00001
2 57954 53.1613 17.7811 0001187 87.9627 272.1511 15.34392046 08
| Epoch (UTC): | 25 May 2026 08:13:40 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 17.7811° |
| argument of perigee: | 87.9627° |
| revolutions per day: | 15.34392046 |
| mean anomaly at epoch: | 272.1511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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