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 55103U 26145.46687169 +.00000000 +00000-0 +42197-3 0 00008
2 55103 97.3253 215.9275 0009436 150.4222 209.7564 15.48510044 09
| Epoch (UTC): | 25 May 2026 11:12:17 |
| Eccentricity: | 0.0009436 |
| inclination: | 97.3253° |
| perigee height: | 415 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 215.9275° |
| argument of perigee: | 150.4222° |
| revolutions per day: | 15.48510044 |
| mean anomaly at epoch: | 209.7564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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