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 27844U 26145.48744789 +.00000000 +00000-0 +12520-3 0 00000
2 27844 98.6738 154.3320 0008361 248.7369 111.2917 14.24319547 05
| Epoch (UTC): | 25 May 2026 11:41:55 |
| Eccentricity: | 0.0008361 |
| inclination: | 98.6738° |
| perigee height: | 805 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 154.3320° |
| argument of perigee: | 248.7369° |
| revolutions per day: | 14.24319547 |
| mean anomaly at epoch: | 111.2917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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