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 29228U 26161.95381397 +.00000000 +00000-0 +12595-3 0 00002
2 29228 69.9338 355.6885 0006639 296.5996 63.4489 15.13189359 02
| Epoch (UTC): | 10 June 2026 22:53:29 |
| Eccentricity: | 0.0006639 |
| inclination: | 69.9338° |
| perigee height: | 522 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 355.6885° |
| argument of perigee: | 296.5996° |
| revolutions per day: | 15.13189359 |
| mean anomaly at epoch: | 63.4489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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