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 53743U 26145.40552259 +.00000000 +00000-0 -15800-4 0 00004
2 53743 53.2136 279.8170 0001195 81.7110 278.4017 15.08837546 08
| Epoch (UTC): | 25 May 2026 09:43:57 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.8170° |
| argument of perigee: | 81.7110° |
| revolutions per day: | 15.08837546 |
| mean anomaly at epoch: | 278.4017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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