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 26076.18418013 +.00000000 +00000-0 +94425-4 0 00009
2 27561 98.4709 295.1527 0045222 54.9209 305.6217 14.58496121 00
| Epoch (UTC): | 17 March 2026 04:25:13 |
| Eccentricity: | 0.0045222 |
| inclination: | 98.4709° |
| perigee height: | 666 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 295.1527° |
| argument of perigee: | 54.9209° |
| revolutions per day: | 14.58496121 |
| mean anomaly at epoch: | 305.6217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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