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 27846U 26150.72127020 +.00000000 +00000-0 +13807-3 0 00007
2 27846 98.6846 159.4188 0008612 206.2922 153.7821 14.23951930 00
| Epoch (UTC): | 30 May 2026 17:18:37 |
| Eccentricity: | 0.0008612 |
| inclination: | 98.6846° |
| perigee height: | 806 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 159.4188° |
| argument of perigee: | 206.2922° |
| revolutions per day: | 14.23951930 |
| mean anomaly at epoch: | 153.7821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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