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 22888U 93070A 25109.34334402 .00000103 00000-0 91804-4 0 9997
2 22888 82.9540 34.8970 0046863 291.0096 191.8567 13.75130964576007
| Epoch (UTC): | 19 April 2025 08:14:24 |
| Eccentricity: | 0.0046863 |
| inclination: | 82.9540° |
| perigee height: | 947 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 34.8970° |
| argument of perigee: | 291.0096° |
| revolutions per day: | 13.75130964 |
| mean anomaly at epoch: | 191.8567° |
| orbit number at epoch: | 57600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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