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 22009U 92037A 25118.02562986 -.00000245 00000-0 00000-0 0 9991
2 22009 13.9477 12.6148 0007215 31.1384 162.5425 0.98813491 21048
| Epoch (UTC): | 28 April 2025 00:36:54 |
| Eccentricity: | 0.0007215 |
| inclination: | 13.9477° |
| perigee height: | 36169 km |
| apogee height: | 36231 km |
| right ascension of ascending node: | 12.6148° |
| argument of perigee: | 31.1384° |
| revolutions per day: | 0.98813491 |
| mean anomaly at epoch: | 162.5425° |
| orbit number at epoch: | 2104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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