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 17528U 26072.96898116 +.00000000 +00000-0 +24139-3 0 00003
2 17528 97.4034 78.0250 0144230 0.2691 359.8561 14.54496825 01
| Epoch (UTC): | 13 March 2026 23:15:19 |
| Eccentricity: | 0.0144230 |
| inclination: | 97.4034° |
| perigee height: | 609 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 78.0250° |
| argument of perigee: | 0.2691° |
| revolutions per day: | 14.54496825 |
| mean anomaly at epoch: | 359.8561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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