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 27848U 26145.46453734 +.00000000 +00000-0 +11605-3 0 00002
2 27848 98.6770 154.0402 0008192 270.2413 89.7827 14.23606827 03
| Epoch (UTC): | 25 May 2026 11:08:56 |
| Eccentricity: | 0.0008192 |
| inclination: | 98.6770° |
| perigee height: | 807 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 154.0402° |
| argument of perigee: | 270.2413° |
| revolutions per day: | 14.23606827 |
| mean anomaly at epoch: | 89.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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