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 55787U 26145.06755266 +.00000000 +00000-0 +25476-4 0 00008
2 55787 69.9997 12.0117 0002728 270.3300 89.7546 14.98332729 06
| Epoch (UTC): | 25 May 2026 01:37:16 |
| Eccentricity: | 0.0002728 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 12.0117° |
| argument of perigee: | 270.3300° |
| revolutions per day: | 14.98332729 |
| mean anomaly at epoch: | 89.7546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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