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 22219U 92076A 25197.95808698 .00000003 00000-0 26434-4 0 9993
2 22219 71.0610 150.8341 0018893 207.3740 152.6389 14.14038171685055
| Epoch (UTC): | 16 July 2025 22:59:38 |
| Eccentricity: | 0.0018893 |
| inclination: | 71.0610° |
| perigee height: | 832 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 150.8341° |
| argument of perigee: | 207.3740° |
| revolutions per day: | 14.14038171 |
| mean anomaly at epoch: | 152.6389° |
| orbit number at epoch: | 68505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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