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 26548U 26155.10879455 +.00000000 +00000-0 +21238-3 0 00005
2 26548 64.5451 167.3954 0042083 292.4494 67.2167 15.01579364 08
| Epoch (UTC): | 04 June 2026 02:36:39 |
| Eccentricity: | 0.0042083 |
| inclination: | 64.5451° |
| perigee height: | 533 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 167.3954° |
| argument of perigee: | 292.4494° |
| revolutions per day: | 15.01579364 |
| mean anomaly at epoch: | 67.2167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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