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 67150U 26145.32025530 +.00000000 +00000-0 +42556-3 0 00005
2 67150 51.9022 104.2858 0000812 58.8801 301.2240 14.79958202 08
| Epoch (UTC): | 25 May 2026 07:41:10 |
| Eccentricity: | 0.0000812 |
| inclination: | 51.9022° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 104.2858° |
| argument of perigee: | 58.8801° |
| revolutions per day: | 14.79958202 |
| mean anomaly at epoch: | 301.2240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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