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 54208U 26144.97085039 +.00000000 +00000-0 -34251-3 0 00009
2 54208 53.2159 346.7300 0001807 90.5770 269.5429 15.08799616 02
| Epoch (UTC): | 24 May 2026 23:18:01 |
| Eccentricity: | 0.0001807 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 346.7300° |
| argument of perigee: | 90.5770° |
| revolutions per day: | 15.08799616 |
| mean anomaly at epoch: | 269.5429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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