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 54788U 26145.41055361 +.00000000 +00000-0 +46024-4 0 00008
2 54788 53.2127 44.5738 0001598 86.8290 273.2885 15.08835103 00
| Epoch (UTC): | 25 May 2026 09:51:11 |
| Eccentricity: | 0.0001598 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.5738° |
| argument of perigee: | 86.8290° |
| revolutions per day: | 15.08835103 |
| mean anomaly at epoch: | 273.2885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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