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 26088.03885231 +.00000000 +00000-0 +17539-3 0 00003
2 27612 64.5544 210.4860 0056190 260.0106 99.4657 14.85316322 00
| Epoch (UTC): | 29 March 2026 00:55:56 |
| Eccentricity: | 0.0056190 |
| inclination: | 64.5544° |
| perigee height: | 573 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 210.4860° |
| argument of perigee: | 260.0106° |
| revolutions per day: | 14.85316322 |
| mean anomaly at epoch: | 99.4657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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