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 53434U 26145.66668980 +.00000000 +00000-0 +38959-2 0 00005
2 53434 53.2169 100.6021 0000896 141.2966 49.6986 15.75223625 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000896 |
| inclination: | 53.2169° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 100.6021° |
| argument of perigee: | 141.2966° |
| revolutions per day: | 15.75223625 |
| mean anomaly at epoch: | 49.6986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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