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 27610U 26044.72675323 +.00000000 +00000-0 +48114-4 0 00002
2 27610 64.5598 161.0338 0266678 109.3920 0.3186 14.29502875 07
| Epoch (UTC): | 13 February 2026 17:26:31 |
| Eccentricity: | 0.0266678 |
| inclination: | 64.5598° |
| perigee height: | 602 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 161.0338° |
| argument of perigee: | 109.3920° |
| revolutions per day: | 14.29502875 |
| mean anomaly at epoch: | 0.3186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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