SPARK 2 is a payload in SSO orbit, operated by Shanghai Engineering Center for Microsatellites, SIMIT, launched 2016.
| Orbit class | SSO |
| Inclination | 98.5499° |
| Eccentricity | 0.0024017 |
| Period | 98.7 min |
| Apogee | 713 km |
| Perigee | 679 km |
| Mean motion | 14.59185973 rev/day |
| RAAN | 178.3114° |
| Arg of perigee | 263.2427° |
| Mean anomaly | 96.6038° |
| B* | 1.0462e-4 |
| Rev at epoch | 50,700 |
1 41901U 16081D 26187.95108801 .00000444 00000-0 10462-3 0 99952 41901 98.5499 178.3114 0024017 263.2427 96.6038 14.59185973507002{
"OBJECT_NAME": "SPARK 2",
"OBJECT_ID": "2016-081D",
"EPOCH": "2026-07-06T22:49:34.004+00:00",
"MEAN_MOTION": 14.59185973,
"ECCENTRICITY": 0.0024017,
"INCLINATION": 98.5499,
"RA_OF_ASC_NODE": 178.3114,
"ARG_OF_PERICENTER": 263.2427,
"MEAN_ANOMALY": 96.6038,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41901,
"REV_AT_EPOCH": 50700,
"BSTAR": 0.00010462,
"MEAN_MOTION_DOT": 0.00000444,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | SPARK 2 |
| Operator | Shanghai Engineering Center for Microsatellites, SIMITHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | China |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |