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 23088U 94023B 25192.51070498 -.00000093 00000-0 -23574-4 0 9991
2 23088 70.9985 217.3659 0005544 291.0155 69.0374 14.14973617611971
| Epoch (UTC): | 11 July 2025 12:15:24 |
| Eccentricity: | 0.0005544 |
| inclination: | 70.9985° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 217.3659° |
| argument of perigee: | 291.0155° |
| revolutions per day: | 14.14973617 |
| mean anomaly at epoch: | 69.0374° |
| orbit number at epoch: | 61197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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