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 43263U 26045.95620051 +.00000000 +00000-0 +36618-3 0 00003
2 43263 97.6940 54.8281 0039441 21.3459 338.9387 14.80054209 02
| Epoch (UTC): | 14 February 2026 22:56:55 |
| Eccentricity: | 0.0039441 |
| inclination: | 97.6940° |
| perigee height: | 602 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 54.8281° |
| argument of perigee: | 21.3459° |
| revolutions per day: | 14.80054209 |
| mean anomaly at epoch: | 338.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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