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 data is extracted from the following two-line orbital elements,
1 12091U 80099A 25115.54203699 .00000105 00000-0 93741-4 0 9995
2 12091 82.9387 313.2188 0034315 145.0521 278.7184 13.74680464225371
| Epoch (UTC): | 25 April 2025 13:00:31 |
| Eccentricity: | 0.0034315 |
| inclination: | 82.9387° |
| perigee height: | 957 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 313.2188° |
| argument of perigee: | 145.0521° |
| revolutions per day: | 13.74680464 |
| mean anomaly at epoch: | 278.7184° |
| orbit number at epoch: | 22537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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