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 12645U 26071.13929814 +.00000000 +00000-0 +62665-4 0 00003
2 12645 81.2169 303.3158 0063642 127.0642 233.6376 14.18959773 07
| Epoch (UTC): | 12 March 2026 03:20:35 |
| Eccentricity: | 0.0063642 |
| inclination: | 81.2169° |
| perigee height: | 783 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 303.3158° |
| argument of perigee: | 127.0642° |
| revolutions per day: | 14.18959773 |
| mean anomaly at epoch: | 233.6376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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