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 39271U 13055G 25039.60136275 .12343816 -98682-6 19828-3 0 9994
2 39271 80.8811 140.2461 0019365 229.2526 242.6684 16.46677559602073
Epoch (UTC): | 08 February 2025 14:25:57 |
Eccentricity: | 0.0019365 |
inclination: | 80.8811° |
perigee height: | 135 km |
apogee height: | 161 km |
right ascension of ascending node: | 140.2461° |
argument of perigee: | 229.2526° |
revolutions per day: | 16.46677559 |
mean anomaly at epoch: | 242.6684° |
orbit number at epoch: | 60207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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