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 55797U 26145.35109703 +.00000000 +00000-0 +98371-4 0 00004
2 55797 87.9167 279.0244 0001833 95.7150 264.4193 13.20770083 03
| Epoch (UTC): | 25 May 2026 08:25:34 |
| Eccentricity: | 0.0001833 |
| inclination: | 87.9167° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0244° |
| argument of perigee: | 95.7150° |
| revolutions per day: | 13.20770083 |
| mean anomaly at epoch: | 264.4193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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