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 54077U 26145.23773584 +.00000000 +00000-0 +40871-3 0 00006
2 54077 53.2108 336.1182 0001950 91.1201 269.0014 15.08802135 02
| Epoch (UTC): | 25 May 2026 05:42:20 |
| Eccentricity: | 0.0001950 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 336.1182° |
| argument of perigee: | 91.1201° |
| revolutions per day: | 15.08802135 |
| mean anomaly at epoch: | 269.0014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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