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 is defined by the following mean orbital elements,
1 22787U 26144.73389730 +.00000000 +00000-0 +00000-0 0 00006
2 22787 11.8870 3.6853 0007990 2.2920 169.2662 1.00277887 00
| Epoch (UTC): | 24 May 2026 17:36:48 |
| Eccentricity: | 0.0007990 |
| inclination: | 11.8870° |
| perigee height: | 35751 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 3.6853° |
| argument of perigee: | 2.2920° |
| revolutions per day: | 1.00277887 |
| mean anomaly at epoch: | 169.2662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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