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 54801U 26145.18650713 +.00000000 +00000-0 -34358-3 0 00007
2 54801 53.2125 60.2715 0001364 96.5752 263.5395 15.08852525 01
| Epoch (UTC): | 25 May 2026 04:28:34 |
| Eccentricity: | 0.0001364 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 60.2715° |
| argument of perigee: | 96.5752° |
| revolutions per day: | 15.08852525 |
| mean anomaly at epoch: | 263.5395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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