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 26145.66150002 +.00000000 +00000-0 +10049-3 0 00002
2 26998 74.0676 280.3708 0000282 152.4038 207.7162 14.95228088 01
| Epoch (UTC): | 25 May 2026 15:52:33 |
| Eccentricity: | 0.0000282 |
| inclination: | 74.0676° |
| perigee height: | 581 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 280.3708° |
| argument of perigee: | 152.4038° |
| revolutions per day: | 14.95228088 |
| mean anomaly at epoch: | 207.7162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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