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 26998U 26088.18535031 +.00000000 +00000-0 +18560-3 0 00000
2 26998 74.0690 36.0776 0002768 250.6198 109.4688 14.95087854 02
| Epoch (UTC): | 29 March 2026 04:26:54 |
| Eccentricity: | 0.0002768 |
| inclination: | 74.0690° |
| perigee height: | 580 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 36.0776° |
| argument of perigee: | 250.6198° |
| revolutions per day: | 14.95087854 |
| mean anomaly at epoch: | 109.4688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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