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 61615U 26145.58062154 +.00000000 +00000-0 +18300-3 0 00006
2 61615 97.5203 166.4356 0004092 71.9280 288.2390 15.01016650 07
| Epoch (UTC): | 25 May 2026 13:56:05 |
| Eccentricity: | 0.0004092 |
| inclination: | 97.5203° |
| perigee height: | 561 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 166.4356° |
| argument of perigee: | 71.9280° |
| revolutions per day: | 15.01016650 |
| mean anomaly at epoch: | 288.2390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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