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 61687U 26145.63284053 +.00000000 +00000-0 +11892-4 0 00005
2 61687 53.1600 7.3111 0000818 81.3290 278.7821 15.69714873 04
| Epoch (UTC): | 25 May 2026 15:11:17 |
| Eccentricity: | 0.0000818 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 7.3111° |
| argument of perigee: | 81.3290° |
| revolutions per day: | 15.69714873 |
| mean anomaly at epoch: | 278.7821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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