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 02826U 26145.57268707 +.00000000 +00000-0 +10759-2 0 00005
2 02826 69.9161 93.7098 0001310 261.2249 98.8750 14.77338963 07
| Epoch (UTC): | 25 May 2026 13:44:40 |
| Eccentricity: | 0.0001310 |
| inclination: | 69.9161° |
| perigee height: | 637 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 93.7098° |
| argument of perigee: | 261.2249° |
| revolutions per day: | 14.77338963 |
| mean anomaly at epoch: | 98.8750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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