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 26106.52703389 +.00000000 +00000-0 +91279-4 0 00006
2 27848 98.6796 115.6194 0010021 29.7735 330.4012 14.23587215 01
| Epoch (UTC): | 16 April 2026 12:38:55 |
| Eccentricity: | 0.0010021 |
| inclination: | 98.6796° |
| perigee height: | 806 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 115.6194° |
| argument of perigee: | 29.7735° |
| revolutions per day: | 14.23587215 |
| mean anomaly at epoch: | 330.4012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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