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 46359U 26145.58335647 +.00000000 +00000-0 +66774-3 0 00002
2 46359 53.0185 252.5275 0005618 334.3945 300.5547 15.81952991 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005618 |
| inclination: | 53.0185° |
| perigee height: | 321 km |
| apogee height: | 329 km |
| right ascension of ascending node: | 252.5275° |
| argument of perigee: | 334.3945° |
| revolutions per day: | 15.81952991 |
| mean anomaly at epoch: | 300.5547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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