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 55054U 26145.43163341 +.00000000 +00000-0 +18969-3 0 00001
2 55054 97.3235 203.1552 0008956 202.9470 157.1371 15.29001229 06
| Epoch (UTC): | 25 May 2026 10:21:33 |
| Eccentricity: | 0.0008956 |
| inclination: | 97.3235° |
| perigee height: | 473 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 203.1552° |
| argument of perigee: | 202.9470° |
| revolutions per day: | 15.29001229 |
| mean anomaly at epoch: | 157.1371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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