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 53394U 26145.36037133 +.00000000 +00000-0 +86077-4 0 00003
2 53394 53.2157 129.5410 0001062 82.9261 277.1852 15.08847211 07
| Epoch (UTC): | 25 May 2026 08:38:56 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 129.5410° |
| argument of perigee: | 82.9261° |
| revolutions per day: | 15.08847211 |
| mean anomaly at epoch: | 277.1852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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