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 22698U 93041A 25322.33557661 .00000295 00000-0 11720-3 0 9994
2 22698 89.4990 72.4372 0089233 154.8215 205.7369 14.24119646682189
| Epoch (UTC): | 18 November 2025 08:03:13 |
| Eccentricity: | 0.0089233 |
| inclination: | 89.4990° |
| perigee height: | 747 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 72.4372° |
| argument of perigee: | 154.8215° |
| revolutions per day: | 14.24119646 |
| mean anomaly at epoch: | 205.7369° |
| orbit number at epoch: | 68218 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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