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 66361U 26145.51346830 +.00000000 +00000-0 +30325-3 0 00009
2 66361 53.1607 235.1939 0000295 24.1479 335.9536 15.31704237 08
| Epoch (UTC): | 25 May 2026 12:19:23 |
| Eccentricity: | 0.0000295 |
| inclination: | 53.1607° |
| perigee height: | 471 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.1939° |
| argument of perigee: | 24.1479° |
| revolutions per day: | 15.31704237 |
| mean anomaly at epoch: | 335.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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