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 04589U 26159.04467388 +.00000000 +00000-0 +95826-4 0 00006
2 04589 74.0605 10.7111 0019516 120.0084 240.3013 14.43351077 06
| Epoch (UTC): | 08 June 2026 01:04:19 |
| Eccentricity: | 0.0019516 |
| inclination: | 74.0605° |
| perigee height: | 734 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 10.7111° |
| argument of perigee: | 120.0084° |
| revolutions per day: | 14.43351077 |
| mean anomaly at epoch: | 240.3013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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