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 02834U 26133.35105318 +.00000000 +00000-0 +38744-4 0 00001
2 02834 69.9725 207.6441 0010120 258.2596 101.7375 13.96187241 08
| Epoch (UTC): | 13 May 2026 08:25:30 |
| Eccentricity: | 0.0010120 |
| inclination: | 69.9725° |
| perigee height: | 900 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 207.6441° |
| argument of perigee: | 258.2596° |
| revolutions per day: | 13.96187241 |
| mean anomaly at epoch: | 101.7375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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