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 26145.06427396 +.00000000 +00000-0 +74461-4 0 00002
2 27612 64.5555 33.4273 0054262 251.4504 108.0704 14.85427081 02
| Epoch (UTC): | 25 May 2026 01:32:33 |
| Eccentricity: | 0.0054262 |
| inclination: | 64.5555° |
| perigee height: | 574 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 33.4273° |
| argument of perigee: | 251.4504° |
| revolutions per day: | 14.85427081 |
| mean anomaly at epoch: | 108.0704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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