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 53829U 26145.21415211 +.00000000 +00000-0 +47122-4 0 00005
2 53829 53.2128 320.6121 0001210 87.7864 272.3267 15.08837943 06
| Epoch (UTC): | 25 May 2026 05:08:22 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 320.6121° |
| argument of perigee: | 87.7864° |
| revolutions per day: | 15.08837943 |
| mean anomaly at epoch: | 272.3267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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