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 11289U 26087.98074007 +.00000000 +00000-0 +11052-3 0 00004
2 11289 81.2429 274.8097 0076052 131.3132 229.4620 14.12102672 01
| Epoch (UTC): | 28 March 2026 23:32:15 |
| Eccentricity: | 0.0076052 |
| inclination: | 81.2429° |
| perigee height: | 797 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 274.8097° |
| argument of perigee: | 131.3132° |
| revolutions per day: | 14.12102672 |
| mean anomaly at epoch: | 229.4620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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