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 23494U 26064.81458979 +.00000000 +00000-0 -96970-1 0 00007
2 23494 64.9315 196.4126 0283459 63.7967 86.3835 11.69211143 02
| Epoch (UTC): | 05 March 2026 19:33:00 |
| Eccentricity: | 0.0283459 |
| inclination: | 64.9315° |
| perigee height: | 1589 km |
| apogee height: | 2054 km |
| right ascension of ascending node: | 196.4126° |
| argument of perigee: | 63.7967° |
| revolutions per day: | 11.69211143 |
| mean anomaly at epoch: | 86.3835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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