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 61200U 26145.33161757 +.00000000 +00000-0 +22473-4 0 00005
2 61200 53.1583 158.6394 0000845 63.7386 296.3719 15.69703021 03
| Epoch (UTC): | 25 May 2026 07:57:31 |
| Eccentricity: | 0.0000845 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.6394° |
| argument of perigee: | 63.7386° |
| revolutions per day: | 15.69703021 |
| mean anomaly at epoch: | 296.3719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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