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 61701U 26145.42852426 +.00000000 +00000-0 +32064-5 0 00009
2 61701 53.1601 157.9886 0001135 83.5988 276.5144 15.34383211 08
| Epoch (UTC): | 25 May 2026 10:17:04 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.9886° |
| argument of perigee: | 83.5988° |
| revolutions per day: | 15.34383211 |
| mean anomaly at epoch: | 276.5144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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