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 61915U 26145.51123015 +.00000000 +00000-0 +52236-3 0 00002
2 61915 42.9984 207.6613 0001595 268.5903 91.4766 15.27590382 03
| Epoch (UTC): | 25 May 2026 12:16:10 |
| Eccentricity: | 0.0001595 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.6613° |
| argument of perigee: | 268.5903° |
| revolutions per day: | 15.27590382 |
| mean anomaly at epoch: | 91.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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