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 27004U 26053.72208338 +.00000000 +00000-0 +29359-4 0 00007
2 27004 99.7986 228.4472 0020576 76.7731 301.2802 13.70257162 03
| Epoch (UTC): | 22 February 2026 17:19:48 |
| Eccentricity: | 0.0020576 |
| inclination: | 99.7986° |
| perigee height: | 983 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 228.4472° |
| argument of perigee: | 76.7731° |
| revolutions per day: | 13.70257162 |
| mean anomaly at epoch: | 301.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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