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 27601U 26021.54088205 +.00000000 +00000-0 +23634-3 0 00003
2 27601 98.3121 343.7264 0069304 302.7616 170.5110 14.33718702 09
| Epoch (UTC): | 21 January 2026 12:58:52 |
| Eccentricity: | 0.0069304 |
| inclination: | 98.3121° |
| perigee height: | 730 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 343.7264° |
| argument of perigee: | 302.7616° |
| revolutions per day: | 14.33718702 |
| mean anomaly at epoch: | 170.5110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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