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 55673U 26145.50936333 +.00000000 +00000-0 -88526-5 0 00004
2 55673 69.9987 330.6736 0002841 265.9914 94.0920 14.98327605 04
| Epoch (UTC): | 25 May 2026 12:13:28 |
| Eccentricity: | 0.0002841 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.6736° |
| argument of perigee: | 265.9914° |
| revolutions per day: | 14.98327605 |
| mean anomaly at epoch: | 94.0920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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