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 27560U 26106.99762402 +.00000000 +00000-0 +13554-3 0 00008
2 27560 98.4487 322.4733 0037461 205.4320 261.6489 14.61742626 08
| Epoch (UTC): | 16 April 2026 23:56:34 |
| Eccentricity: | 0.0037461 |
| inclination: | 98.4487° |
| perigee height: | 661 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 322.4733° |
| argument of perigee: | 205.4320° |
| revolutions per day: | 14.61742626 |
| mean anomaly at epoch: | 261.6489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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