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 22285U 92093B 25198.26249714 -.00000240 00000-0 -98478-4 0 9990
2 22285 71.0218 138.4734 0006369 294.1846 65.8610 14.15400938679843
| Epoch (UTC): | 17 July 2025 06:17:59 |
| Eccentricity: | 0.0006369 |
| inclination: | 71.0218° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 138.4734° |
| argument of perigee: | 294.1846° |
| revolutions per day: | 14.15400938 |
| mean anomaly at epoch: | 65.8610° |
| orbit number at epoch: | 67984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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