▸Orbital parameters

Orbit class	SSO
Inclination	97.4484°
Eccentricity	0.0007256
Period	94.9 min
Apogee	518 km
Perigee	508 km
Mean motion	15.17654079 rev/day
RAAN	145.3419°
Arg of perigee	19.0343°
Mean anomaly	341.1160°
B*	3.1523e-4
Rev at epoch	1,484

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68470U 26067BG 26187.38446575 .00006284 00000-0 31523-3 0 9999

2 68470 97.4484 145.3419 0007256 19.0343 341.1160 15.17654079 14848

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LUNA-2",
  "OBJECT_ID": "2026-067BG",
  "EPOCH": "2026-07-06T09:13:37.841+00:00",
  "MEAN_MOTION": 15.17654079,
  "ECCENTRICITY": 0.00072564,
  "INCLINATION": 97.4484,
  "RA_OF_ASC_NODE": 145.3419,
  "ARG_OF_PERICENTER": 19.0343,
  "MEAN_ANOMALY": 341.116,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68470,
  "REV_AT_EPOCH": 1484,
  "BSTAR": 0.00031523361,
  "MEAN_MOTION_DOT": 0.00006284,
  "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	LUNA-2
Operator	ASELSAN A.S.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia 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/68470

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