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 53943U 26145.46784955 +.00000000 +00000-0 +30064-3 0 00009
2 53943 34.9917 67.7880 0004019 168.1574 191.9235 15.23321918 06
| Epoch (UTC): | 25 May 2026 11:13:42 |
| Eccentricity: | 0.0004019 |
| inclination: | 34.9917° |
| perigee height: | 493 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 67.7880° |
| argument of perigee: | 168.1574° |
| revolutions per day: | 15.23321918 |
| mean anomaly at epoch: | 191.9235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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