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 61205U 26145.30218168 +.00000000 +00000-0 +19638-4 0 00005
2 61205 53.1591 158.4372 0001127 67.7761 292.3376 15.69707408 04
| Epoch (UTC): | 25 May 2026 07:15:08 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.4372° |
| argument of perigee: | 67.7761° |
| revolutions per day: | 15.69707408 |
| mean anomaly at epoch: | 292.3376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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