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 22889U 93070B 25073.54463316 .00000107 00000-0 90442-4 0 9998
2 22889 82.9495 13.7107 0048670 221.6423 138.1026 13.78198412576768
| Epoch (UTC): | 14 March 2025 13:04:16 |
| Eccentricity: | 0.0048670 |
| inclination: | 82.9495° |
| perigee height: | 934 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 13.7107° |
| argument of perigee: | 221.6423° |
| revolutions per day: | 13.78198412 |
| mean anomaly at epoch: | 138.1026° |
| orbit number at epoch: | 57676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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