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 22988U 94009A 23088.37888502 -.00000199 00000-0 00000-0 0 9993
2 22988 15.8071 40.1124 0003193 316.2995 236.5215 1.00274527 21179
| Epoch (UTC): | 29 March 2023 09:05:35 |
| Eccentricity: | 0.0003193 |
| inclination: | 15.8071° |
| perigee height: | 35772 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 40.1124° |
| argument of perigee: | 316.2995° |
| revolutions per day: | 1.00274527 |
| mean anomaly at epoch: | 236.5215° |
| orbit number at epoch: | 2117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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