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 25322.31291786 .00000087 00000-0 73968-4 0 9990
2 22888 82.9517 237.2568 0049360 56.6553 59.5975 13.75153854605044
| Epoch (UTC): | 18 November 2025 07:30:36 |
| Eccentricity: | 0.0049360 |
| inclination: | 82.9517° |
| perigee height: | 945 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 237.2568° |
| argument of perigee: | 56.6553° |
| revolutions per day: | 13.75153854 |
| mean anomaly at epoch: | 59.5975° |
| orbit number at epoch: | 60504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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