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 22988U 26145.53843933 +.00000000 +00000-0 +00000-0 0 00008
2 22988 17.5949 27.9428 0000875 269.7485 270.7534 0.98723650 07
| Epoch (UTC): | 25 May 2026 12:55:21 |
| Eccentricity: | 0.0000875 |
| inclination: | 17.5949° |
| perigee height: | 36223 km |
| apogee height: | 36230 km |
| right ascension of ascending node: | 27.9428° |
| argument of perigee: | 269.7485° |
| revolutions per day: | 0.98723650 |
| mean anomaly at epoch: | 270.7534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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