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 27618U 26153.99886052 +.00000000 +00000-0 +00000-0 0 00001
2 27618 65.4389 316.1332 0003067 156.6610 210.6149 2.13100014 06
| Epoch (UTC): | 02 June 2026 23:58:21 |
| Eccentricity: | 0.0003067 |
| inclination: | 65.4389° |
| perigee height: | 19122 km |
| apogee height: | 19138 km |
| right ascension of ascending node: | 316.1332° |
| argument of perigee: | 156.6610° |
| revolutions per day: | 2.13100014 |
| mean anomaly at epoch: | 210.6149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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