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 63708U 26145.39918205 +.00000000 +00000-0 +69276-3 0 00005
2 63708 53.1603 223.2831 0000373 105.8085 254.2957 15.30210337 04
| Epoch (UTC): | 25 May 2026 09:34:49 |
| Eccentricity: | 0.0000373 |
| inclination: | 53.1603° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 223.2831° |
| argument of perigee: | 105.8085° |
| revolutions per day: | 15.30210337 |
| mean anomaly at epoch: | 254.2957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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