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 22803U 93059B 25193.35520872 .00000147 00000-0 96570-4 0 9996
2 22803 70.9897 157.9247 0018580 222.2362 137.7331 14.17181147645749
Epoch (UTC): | 12 July 2025 08:31:30 |
Eccentricity: | 0.0018580 |
inclination: | 70.9897° |
perigee height: | 821 km |
apogee height: | 848 km |
right ascension of ascending node: | 157.9247° |
argument of perigee: | 222.2362° |
revolutions per day: | 14.17181147 |
mean anomaly at epoch: | 137.7331° |
orbit number at epoch: | 64574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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