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 54785U 26145.33695432 +.00000000 +00000-0 -21533-5 0 00005
2 54785 53.2142 4.9074 0001282 76.3764 283.7371 15.08837993 02
| Epoch (UTC): | 25 May 2026 08:05:12 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 4.9074° |
| argument of perigee: | 76.3764° |
| revolutions per day: | 15.08837993 |
| mean anomaly at epoch: | 283.7371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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