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 61545U 26145.35541709 +.00000000 +00000-0 +77676-4 0 00003
2 61545 53.1617 17.9229 0001249 101.8674 258.2467 15.30181611 00
| Epoch (UTC): | 25 May 2026 08:31:48 |
| Eccentricity: | 0.0001249 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.9229° |
| argument of perigee: | 101.8674° |
| revolutions per day: | 15.30181611 |
| mean anomaly at epoch: | 258.2467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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