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 27612U 26134.15768578 +.00000000 +00000-0 +68987-4 0 00006
2 27612 64.5547 67.2925 0054728 253.1349 106.3752 14.85413766 04
| Epoch (UTC): | 14 May 2026 03:47:04 |
| Eccentricity: | 0.0054728 |
| inclination: | 64.5547° |
| perigee height: | 574 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 67.2925° |
| argument of perigee: | 253.1349° |
| revolutions per day: | 14.85413766 |
| mean anomaly at epoch: | 106.3752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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