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 27940U 26088.10183433 +.00000000 +00000-0 +12962-3 0 00005
2 27940 98.3837 263.9541 0011949 247.2321 112.7621 14.69396438 00
| Epoch (UTC): | 29 March 2026 02:26:38 |
| Eccentricity: | 0.0011949 |
| inclination: | 98.3837° |
| perigee height: | 655 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 263.9541° |
| argument of perigee: | 247.2321° |
| revolutions per day: | 14.69396438 |
| mean anomaly at epoch: | 112.7621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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