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 61875U 26145.50295779 +.00000000 +00000-0 +89976-5 0 00006
2 61875 53.1587 337.2652 0000938 84.3026 275.8099 15.69714719 09
| Epoch (UTC): | 25 May 2026 12:04:15 |
| Eccentricity: | 0.0000938 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.2652° |
| argument of perigee: | 84.3026° |
| revolutions per day: | 15.69714719 |
| mean anomaly at epoch: | 275.8099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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