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 13295U 26150.54065544 +.00000000 +00000-0 +00000-0 0 00000
2 13295 62.1940 146.6069 7284623 43.3947 354.8919 2.00279364 00
| Epoch (UTC): | 30 May 2026 12:58:32 |
| Eccentricity: | 0.7284623 |
| inclination: | 62.1940° |
| perigee height: | 841 km |
| apogee height: | 39574 km |
| right ascension of ascending node: | 146.6069° |
| argument of perigee: | 43.3947° |
| revolutions per day: | 2.00279364 |
| mean anomaly at epoch: | 354.8919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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