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 31295U 99025BPD 22181.52860765 -.00000215 00000-0 -12528-3 0 9999
2 31295 98.4324 102.4319 0078192 178.4329 181.7095 13.96193346779002
Epoch (UTC): | 30 June 2022 12:41:11 |
Eccentricity: | 0.0078192 |
inclination: | 98.4324° |
perigee height: | 850 km |
apogee height: | 964 km |
right ascension of ascending node: | 102.4319° |
argument of perigee: | 178.4329° |
revolutions per day: | 13.96193346 |
mean anomaly at epoch: | 181.7095° |
orbit number at epoch: | 77900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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