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 13067U 82013A 25094.04292280 .15183099 -88184-6 34145-3 0 9990
2 13067 81.1376 9.5213 0008476 233.8261 233.6600 16.46050672362621
Epoch (UTC): | 04 April 2025 01:01:48 |
Eccentricity: | 0.0008476 |
inclination: | 81.1376° |
perigee height: | 144 km |
apogee height: | 155 km |
right ascension of ascending node: | 9.5213° |
argument of perigee: | 233.8261° |
revolutions per day: | 16.46050672 |
mean anomaly at epoch: | 233.6600° |
orbit number at epoch: | 36262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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