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 00837U 26110.35622351 +.00000000 +00000-0 +00000-0 0 00008
2 00837 48.7338 123.0086 5863255 256.6246 0.6859 0.23995718 00
| Epoch (UTC): | 20 April 2026 08:32:57 |
| Eccentricity: | 0.5863255 |
| inclination: | 48.7338° |
| perigee height: | 38874 km |
| apogee height: | 167151 km |
| right ascension of ascending node: | 123.0086° |
| argument of perigee: | 256.6246° |
| revolutions per day: | 0.23995718 |
| mean anomaly at epoch: | 0.6859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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