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 00045U 26050.10071470 +.00000000 +00000-0 +73046-4 0 00009
2 00045 66.6943 312.5372 0255461 246.0816 111.3337 14.35873242 06
| Epoch (UTC): | 19 February 2026 02:25:01 |
| Eccentricity: | 0.0255461 |
| inclination: | 66.6943° |
| perigee height: | 590 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 312.5372° |
| argument of perigee: | 246.0816° |
| revolutions per day: | 14.35873242 |
| mean anomaly at epoch: | 111.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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