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 26104.98040801 +.00000000 +00000-0 +73822-4 0 00006
2 26998 74.0697 2.2729 0002243 227.3448 132.7548 14.95147777 04
| Epoch (UTC): | 14 April 2026 23:31:47 |
| Eccentricity: | 0.0002243 |
| inclination: | 74.0697° |
| perigee height: | 580 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 2.2729° |
| argument of perigee: | 227.3448° |
| revolutions per day: | 14.95147777 |
| mean anomaly at epoch: | 132.7548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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