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 49181U 26145.30850573 +.00000000 +00000-0 -29028-5 0 00002
2 49181 69.9993 101.2746 0003285 269.3887 90.6896 14.98332885 01
| Epoch (UTC): | 25 May 2026 07:24:14 |
| Eccentricity: | 0.0003285 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2746° |
| argument of perigee: | 269.3887° |
| revolutions per day: | 14.98332885 |
| mean anomaly at epoch: | 90.6896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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