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 61677U 26145.24518688 +.00000000 +00000-0 +97611-5 0 00009
2 61677 53.1612 94.2792 0001347 86.7034 273.4123 15.34383042 08
| Epoch (UTC): | 25 May 2026 05:53:04 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.2792° |
| argument of perigee: | 86.7034° |
| revolutions per day: | 15.34383042 |
| mean anomaly at epoch: | 273.4123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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