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 61214U 26145.48588980 +.00000000 +00000-0 -33155-4 0 00007
2 61214 53.1628 325.2129 0001506 103.4851 256.6320 15.34396987 08
| Epoch (UTC): | 25 May 2026 11:39:40 |
| Eccentricity: | 0.0001506 |
| inclination: | 53.1628° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.2129° |
| argument of perigee: | 103.4851° |
| revolutions per day: | 15.34396987 |
| mean anomaly at epoch: | 256.6320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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