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 27598U 26053.53726572 +.00000000 +00000-0 +75871-4 0 00009
2 27598 98.8471 25.0648 0008225 317.6222 42.4323 14.29692879 00
| Epoch (UTC): | 22 February 2026 12:53:39 |
| Eccentricity: | 0.0008225 |
| inclination: | 98.8471° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 25.0648° |
| argument of perigee: | 317.6222° |
| revolutions per day: | 14.29692879 |
| mean anomaly at epoch: | 42.4323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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