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 23082.92712715 .00000100 00000-0 88472-4 0 9990
2 22888 82.9495 235.3853 0047050 242.9875 230.8013 13.74997253471682
| Epoch (UTC): | 23 March 2023 22:15:03 |
| Eccentricity: | 0.0047050 |
| inclination: | 82.9495° |
| perigee height: | 947 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 235.3853° |
| argument of perigee: | 242.9875° |
| revolutions per day: | 13.74997253 |
| mean anomaly at epoch: | 230.8013° |
| orbit number at epoch: | 47168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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