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 22287U 92094B 25188.59902923 .00000267 00000-0 32163-4 0 9992
2 22287 82.5224 221.0708 0025273 62.0300 298.3466 14.79799632732272
Epoch (UTC): | 07 July 2025 14:22:36 |
Eccentricity: | 0.0025273 |
inclination: | 82.5224° |
perigee height: | 612 km |
apogee height: | 647 km |
right ascension of ascending node: | 221.0708° |
argument of perigee: | 62.0300° |
revolutions per day: | 14.79799632 |
mean anomaly at epoch: | 298.3466° |
orbit number at epoch: | 73227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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