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 42194U 81053TJ 25046.40404767 .00002695 00000-0 25757-2 0 9996
2 42194 82.8257 90.5624 0201355 91.4820 270.9409 13.71529663560263
| Epoch (UTC): | 15 February 2025 09:41:49 |
| Eccentricity: | 0.0201355 |
| inclination: | 82.8257° |
| perigee height: | 845 km |
| apogee height: | 1142 km |
| right ascension of ascending node: | 90.5624° |
| argument of perigee: | 91.4820° |
| revolutions per day: | 13.71529663 |
| mean anomaly at epoch: | 270.9409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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