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 00273U 26136.14137183 +.00000000 +00000-0 -27657-2 0 00001
2 00273 86.6496 301.7266 0326241 258.3594 98.0530 9.43831109 05
| Epoch (UTC): | 16 May 2026 03:23:34 |
| Eccentricity: | 0.0326241 |
| inclination: | 86.6496° |
| perigee height: | 2771 km |
| apogee height: | 3389 km |
| right ascension of ascending node: | 301.7266° |
| argument of perigee: | 258.3594° |
| revolutions per day: | 9.43831109 |
| mean anomaly at epoch: | 98.0530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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