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 61618U 26145.63179777 +.00000000 +00000-0 +33885-3 0 00000
2 61618 34.9888 339.4890 0005300 161.6868 198.4038 15.22983204 03
| Epoch (UTC): | 25 May 2026 15:09:47 |
| Eccentricity: | 0.0005300 |
| inclination: | 34.9888° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 339.4890° |
| argument of perigee: | 161.6868° |
| revolutions per day: | 15.22983204 |
| mean anomaly at epoch: | 198.4038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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