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 26140.50921257 +.00000000 +00000-0 +35416-4 0 00009
2 00045 66.6934 73.4062 0248685 181.1056 178.9531 14.35948539 07
| Epoch (UTC): | 20 May 2026 12:13:15 |
| Eccentricity: | 0.0248685 |
| inclination: | 66.6934° |
| perigee height: | 594 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 73.4062° |
| argument of perigee: | 181.1056° |
| revolutions per day: | 14.35948539 |
| mean anomaly at epoch: | 178.9531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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