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 25989U 26079.59170771 +.00000000 +00000-0 +00000-0 0 00007
2 25989 64.9328 284.1312 4707488 66.4925 359.9625 0.50125634 03
| Epoch (UTC): | 20 March 2026 14:12:03 |
| Eccentricity: | 0.4707488 |
| inclination: | 64.9328° |
| perigee height: | 29051 km |
| apogee height: | 92076 km |
| right ascension of ascending node: | 284.1312° |
| argument of perigee: | 66.4925° |
| revolutions per day: | 0.50125634 |
| mean anomaly at epoch: | 359.9625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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