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 54797U 26145.47821890 +.00000000 +00000-0 +38192-3 0 00008
2 54797 53.2131 59.2450 0001258 101.1587 258.9547 15.08807473 06
| Epoch (UTC): | 25 May 2026 11:28:38 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.2450° |
| argument of perigee: | 101.1587° |
| revolutions per day: | 15.08807473 |
| mean anomaly at epoch: | 258.9547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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