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 12848U 26159.47191514 +.00000000 +00000-0 +35377-3 0 00009
2 12848 82.4646 296.0549 0459986 225.1756 131.1200 14.58613529 01
| Epoch (UTC): | 08 June 2026 11:19:33 |
| Eccentricity: | 0.0459986 |
| inclination: | 82.4646° |
| perigee height: | 372 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 296.0549° |
| argument of perigee: | 225.1756° |
| revolutions per day: | 14.58613529 |
| mean anomaly at epoch: | 131.1200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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