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 27561U 26159.46748492 +.00000000 +00000-0 +87354-4 0 00002
2 27561 98.4588 19.9575 0044623 155.3496 204.9848 14.58564731 02
| Epoch (UTC): | 08 June 2026 11:13:10 |
| Eccentricity: | 0.0044623 |
| inclination: | 98.4588° |
| perigee height: | 666 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 19.9575° |
| argument of perigee: | 155.3496° |
| revolutions per day: | 14.58564731 |
| mean anomaly at epoch: | 204.9848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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