▸Orbital parameters

Orbit class	SSO
Inclination	97.4246°
Eccentricity	0.0003234
Period	94.5 min
Apogee	499 km
Perigee	494 km
Mean motion	15.23146354 rev/day
RAAN	262.2748°
Arg of perigee	134.7462°
Mean anomaly	225.4038°
B*	3.3250e-4
Rev at epoch	3,350

▸Two-line element set (TLE)

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

1 66777U 25276DR 26188.16290382 .00007785 00000-0 33250-3 0 9994

2 66777 97.4246 262.2748 0003234 134.7462 225.4038 15.23146354 33506

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LUNA-1",
  "OBJECT_ID": "2025-276DR",
  "EPOCH": "2026-07-07T03:54:34.89+00:00",
  "MEAN_MOTION": 15.23146354,
  "ECCENTRICITY": 0.0003234,
  "INCLINATION": 97.4246,
  "RA_OF_ASC_NODE": 262.2748,
  "ARG_OF_PERICENTER": 134.7462,
  "MEAN_ANOMALY": 225.4038,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66777,
  "REV_AT_EPOCH": 3350,
  "BSTAR": 0.0003325,
  "MEAN_MOTION_DOT": 0.00007785,
  "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-1
Operator	ASELSAN A.S.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Nov 28, 2025HIGHvia 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/66777

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