▸Orbital parameters

Orbit class	SSO
Inclination	97.4282°
Eccentricity	0.0003823
Period	95.0 min
Apogee	522 km
Perigee	516 km
Mean motion	15.15659206 rev/day
RAAN	235.6938°
Arg of perigee	210.5456°
Mean anomaly	149.5555°
B*	2.2105e-4
Rev at epoch	41,529

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43768U 18099L 26188.09449705 .00004140 00000-0 22105-3 0 9990

2 43768 97.4282 235.6938 0003823 210.5456 149.5555 15.15659206415292

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AISTECHSAT 2",
  "OBJECT_ID": "2018-099L",
  "EPOCH": "2026-07-07T02:16:04.545+00:00",
  "MEAN_MOTION": 15.15659206,
  "ECCENTRICITY": 0.0003823,
  "INCLINATION": 97.4282,
  "RA_OF_ASC_NODE": 235.6938,
  "ARG_OF_PERICENTER": 210.5456,
  "MEAN_ANOMALY": 149.5555,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43768,
  "REV_AT_EPOCH": 41529,
  "BSTAR": 0.00022105,
  "MEAN_MOTION_DOT": 0.0000414,
  "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.

▸Satellite metadata

Name	AISTECHSAT 2
Operator	Aistech SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Spain
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/43768

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.