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 00965U 26048.41874163 +.00000000 +00000-0 +59945-4 0 00003
2 00965 90.0712 202.0740 0039593 267.9445 145.1231 13.56999344 02
| Epoch (UTC): | 17 February 2026 10:02:59 |
| Eccentricity: | 0.0039593 |
| inclination: | 90.0712° |
| perigee height: | 1017 km |
| apogee height: | 1076 km |
| right ascension of ascending node: | 202.0740° |
| argument of perigee: | 267.9445° |
| revolutions per day: | 13.56999344 |
| mean anomaly at epoch: | 145.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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