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 29522U 26145.61274816 +.00000000 +00000-0 +50621-4 0 00004
2 29522 98.7381 152.6449 0011163 117.2417 242.9895 14.14988735 03
| Epoch (UTC): | 25 May 2026 14:42:21 |
| Eccentricity: | 0.0011163 |
| inclination: | 98.7381° |
| perigee height: | 834 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 152.6449° |
| argument of perigee: | 117.2417° |
| revolutions per day: | 14.14988735 |
| mean anomaly at epoch: | 242.9895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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