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 26152.00751050 +.00000000 +00000-0 +00000-0 0 00005
2 00837 48.7113 121.7716 6047784 256.4160 0.7140 0.24000687 08
| Epoch (UTC): | 01 June 2026 00:10:48 |
| Eccentricity: | 0.6047784 |
| inclination: | 48.7113° |
| perigee height: | 36849 km |
| apogee height: | 169145 km |
| right ascension of ascending node: | 121.7716° |
| argument of perigee: | 256.4160° |
| revolutions per day: | 0.24000687 |
| mean anomaly at epoch: | 0.7140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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