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 12677U 26106.44558367 +.00000000 +00000-0 +00000-0 0 00003
2 12677 8.1149 304.5900 0011130 334.1536 209.8302 0.99554280 06
| Epoch (UTC): | 16 April 2026 10:41:38 |
| Eccentricity: | 0.0011130 |
| inclination: | 8.1149° |
| perigee height: | 35942 km |
| apogee height: | 36036 km |
| right ascension of ascending node: | 304.5900° |
| argument of perigee: | 334.1536° |
| revolutions per day: | 0.99554280 |
| mean anomaly at epoch: | 209.8302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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