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 26150.41193361 +.00000000 +00000-0 +15770-3 0 00002
2 26998 74.0680 270.8067 0000133 65.6229 294.4969 14.95245117 00
| Epoch (UTC): | 30 May 2026 09:53:11 |
| Eccentricity: | 0.0000133 |
| inclination: | 74.0680° |
| perigee height: | 582 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 270.8067° |
| argument of perigee: | 65.6229° |
| revolutions per day: | 14.95245117 |
| mean anomaly at epoch: | 294.4969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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