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 12508U 26139.55779133 +.00000000 +00000-0 +40210-4 0 00001
2 12508 82.9587 248.9769 0038868 92.2378 268.3231 13.76641127 09
| Epoch (UTC): | 19 May 2026 13:23:13 |
| Eccentricity: | 0.0038868 |
| inclination: | 82.9587° |
| perigee height: | 947 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 248.9769° |
| argument of perigee: | 92.2378° |
| revolutions per day: | 13.76641127 |
| mean anomaly at epoch: | 268.3231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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